ANNEX IU.K.

ANNEX IU.K. List referred to in Article 3 of this Regulation

LIST OF DUAL-USE ITEMS

This list implements internationally agreed dual-use controls including the Wassenaar Arrangement, the Missile Technology Control Regime (MTCR), the Nuclear Suppliers' Group (NSG), the Australia Group and the Chemical Weapons Convention (CWC).

CONTENTS

a

Notes

b

Acronyms and abbreviations

c

Definitions

Category 0

Nuclear materials, facilities and equipment

Category 1

Special materials and related equipment

Category 2

Materials processing

Category 3

Electronics

Category 4

Computers

Category 5

Telecommunications and "information security"

Category 6

Sensors and lasers

Category 7

Navigation and avionics

Category 8

Marine

Category 9

Aerospace and propulsion

GENERAL NOTES TO ANNEX I
1.For control of goods which are designed or modified for military use, see the relevant list(s) of controls on military goods maintained by individual Member States. References in this Annex that state "SEE ALSO MILITARY GOODS CONTROLS" refer to the same lists.
2.The object of the controls contained in this Annex should not be defeated by the export of any non-controlled goods (including plant) containing one or more controlled components when the controlled component or components are the principal element of the goods and can feasibly be removed or used for other purposes.
N.B.: In judging whether the controlled component or components are to be considered the principal element, it is necessary to weigh the factors of quantity, value and technological know-how involved and other special circumstances which might establish the controlled component or components as the principal element of the goods being procured.
3.Goods specified in this Annex include both new and used goods.
4.In some instances chemicals are listed by name and CAS number. The list applies to chemicals of the same structural formula (including hydrates) regardless of name or CAS number. CAS numbers are shown to assist in identifying a particular chemical or mixture, irrespective of nomenclature. CAS numbers cannot be used as unique identifiers because some forms of the listed chemical have different CAS numbers, and mixtures containing a listed chemical may also have different CAS numbers.
NUCLEAR TECHNOLOGY NOTE (NTN)

(To be read in conjunction with section E of Category 0.)

The "technology" directly associated with any goods controlled in Category 0 is controlled according to the provisions of Category 0.

"Technology" for the "development", "production" or "use" of goods under control remains under control even when applicable to non-controlled goods.

The approval of goods for export also authorizes the export to the same end-user of the minimum "technology" required for the installation, operation, maintenance and repair of the goods.

Controls on "technology" transfer do not apply to information "in the public domain" or to "basic scientific research".

GENERAL TECHNOLOGY NOTE (GTN)

(To be read in conjunction with section E of Categories 1 to 9.)

The export of "technology" which is "required" for the "development", "production" or "use" of goods controlled in Categories 1 to 9, is controlled according to the provisions of Categories 1 to 9.

"Technology" "required" for the "development", "production" or "use" of goods under control remains under control even when applicable to non-controlled goods.

Controls do not apply to that "technology" which is the minimum necessary for the installation, operation, maintenance (checking) or repair of those goods which are not controlled or whose export has been authorised.

N.B.: This does not release such "technology" specified in 1E002.e., 1E002.f., 8E002.a. and 8E002.b.

Controls on "technology" transfer do not apply to information "in the public domain", to "basic scientific research" or to the minimum necessary information for patent applications.

GENERAL SOFTWARE NOTE (GSN)

(This note overrides any control within section D of Categories 0 to 9.)

Categories 0 to 9 of this list do not control "software" which is any of the following:

EDITORIAL PRACTICES IN THE OFFICIAL JOURNAL OF THE EUROPEAN UNION

In accordance with the rules set out in paragraph 6.5 on page 108 of the Interinstitutional style guide (2015 edition), for texts in English published in the Official Journal of the European Union:

  • a comma is used to separate the whole number from decimals,

whole numbers are presented in series of three, each series being separated by a thin space. The text reproduced in this annex follows the above-described practice.

ACRONYMS AND ABBREVIATIONS USED IN THIS ANNEX

An acronym or abbreviation, when used as a defined term, will be found in 'Definitions of Terms used in this Annex'.

Acronym or meaning abbreviation
ABECAnnular Bearing Engineers Committee
AGMAAmerican Gear Manufacturers' Association
AHRSattitude and heading reference systems
AISIAmerican Iron and Steel Institute
ALUarithmetic logic unit
ANSIAmerican National Standards Institute
ASTMthe American Society for Testing and Materials
ATCair traffic control
AVLISatomic vapour laser isotope separation
CADcomputer-aided-design
CASChemical Abstracts Service
CDUcontrol and display unit
CEPcircular error probable
CNTDcontrolled nucleation thermal deposition
CPUCentral processing unit
CVDchemical vapour deposition
CWchemical warfare
CW (for lasers)continuous wave
DMEdistance measuring equipment
DSdirectionally solidified
EB-PVDelectron beam physical vapour deposition
EBUEuropean Broadcasting Union
ECMelectro-chemical machining
ECRelectron cyclotron resonance
EDMelectrical discharge machines
EEPROMSelectrically erasable programmable read only memory
EIAElectronic Industries Association
EMCelectromagnetic compatibility
ETSIEuropean Telecommunications Standards Institute
FFTFast Fourier Transform
GLONASSglobal navigation satellite system
GPSglobal positioning system
HBThetero-bipolar transistors
HDDRhigh density digital recording
HEMThigh electron mobility transistors
ICAOInternational Civil Aviation Organisation
IECInternational Electro-technical Commission
IEEEInstitute of Electrical and Electronic Engineers
IFOVinstantaneous-field-of-view
ILSinstrument landing system
IRIGinter-range instrumentation group
ISAinternational standard atmosphere
ISARinverse synthetic aperture radar
ISOInternational Organization for Standardization
ITUInternational Telecommunication Union
JISJapanese Industrial Standard
JTJoule-Thomson
LIDARlight detection and ranging
LRUline replaceable unit
MACmessage authentication code
Machratio of speed of an object to speed of sound (after Ernst Mach)
MLISmolecular laser isotopic separation
MLSmicrowave landing systems
MOCVDmetal organic chemical vapour deposition
MRImagnetic resonance imaging
MTBFmean-time-between-failures
Mtopsmillion theoretical operations per second
MTTFmean-time-to-failure
NBCNuclear, Biological and Chemical
NDTnon-destructive test
PARprecision approach radar
PINpersonal identification number
ppmparts per million
PSDpower spectral density
QAMquadrature-amplitude-modulation
RFradio frequency
SACMASuppliers of Advanced Composite Materials Association
SARsynthetic aperture radar
SCsingle crystal
SLARsidelooking airborne radar
SMPTESociety of Motion Picture and Television Engineers
SRAshop replaceable assembly
SRAMstatic random access memory
SRMSACMA Recommended Methods
SSBsingle sideband
SSRsecondary surveillance radar
TCSECtrusted computer system evaluation criteria
TIRtotal indicated reading
UVUltraviolet
UTSultimate tensile strength
VORvery high frequency omni-directional range
YAGyttrium/aluminium garnet
DEFINITIONS OF TERMS USED IN THIS ANNEX

Definitions of terms between 'single quotation marks' are given in a Technical Note to the relevant item.

Definitions of terms between "double quotation marks" are as follows:

N.B.: Category references are given in brackets after the defined term.

"Accuracy" (2 6), usually measured in terms of inaccuracy, means the maximum deviation, positive or negative, of an indicated value from an accepted standard or true value.

"Active flight control systems" (7) are systems that function to prevent undesirable "aircraft" and missile motions or structural loads by autonomously processing outputs from multiple sensors and then providing necessary preventive commands to effect automatic control.

"Active pixel" (6 8) is a minimum (single) element of the solid state array which has a photoelectric transfer function when exposed to light (electromagnetic) radiation.

"Adapted for use in war" (1) means any modification or selection (such as altering purity, shelf life, virulence, dissemination characteristics, or resistance to UV radiation) designed to increase the effectiveness in producing casualties in humans or animals, degrading equipment or damaging crops or the environment.

"Adjusted Peak Performance" (4) is an adjusted peak rate at which "digital computers" perform 64-bit or larger floating point additions and multiplications, and is expressed in Weighted TeraFLOPS (WT) with units of 1012 adjusted floating point operations per second.

N.B.: See Category 4, Technical Note.

"Aircraft" (1 7 9) means a fixed wing, swivel wing, rotary wing (helicopter), tilt rotor or tilt-wing airborne vehicle.

N.B.: See also "civil aircraft".

"Airship" (9) means a power-driven airborne vehicle that is kept buoyant by a body of gas (usually helium, formerly hydrogen) which is lighter than air.

"All compensations available" (2) means after all feasible measures available to the manufacturer to minimise all systematic positioning errors for the particular machine-tool model or measuring errors for the particular coordinate measuring machine are considered.

"Allocated by the ITU" (3 5) means the allocation of frequency bands according to the current edition of the ITU Radio Regulations for primary, permitted and secondary services.

N.B.: Additional and alternative allocations are not included.

"Angular position deviation" (2) means the maximum difference between angular position and the actual, very accurately measured angular position after the workpiece mount of the table has been turned out of its initial position

"Angle random walk" (7) means the angular error build up with time that is due to white noise in angular rate. (IEEE STD 528-2001)

"APP" (4) is equivalent to "Adjusted Peak Performance".

"Asymmetric algorithm" (5) means a cryptographic algorithm using different, mathematically-related keys for encryption and decryption.

N.B.: A common use of "asymmetric algorithms" is key management.

"Automatic target tracking" (6) means a processing technique that automatically determines and provides as output an extrapolated value of the most probable position of the target in real time.

"Average output power" (6) means the total "laser" output energy, in joules, divided by the period over which a series of consecutive pulses is emitted, in seconds. For a series of uniformly spaced pulses it is equal to the total "laser" output energy in a single pulse, in joules, multiplied by the pulse frequency of the "laser", in Hertz.

"Basic gate propagation delay time" (3) means the propagation delay time value corresponding to the basic gate used in a "monolithic integrated circuit". For a 'family' of "monolithic integrated circuits", this may be specified either as the propagation delay time per typical gate within the given 'family' or as the typical propagation delay time per gate within the given 'family'.

N.B. 1: "Basic gate propagation delay time" is not to be confused with the input/output delay time of a complex "monolithic integrated circuit".
N.B. 2: 'Family' consists of all integrated circuits to which all of the following are applied as their manufacturing methodology and specifications except their respective functions:
a.

The common hardware and software architecture;

b.

The common design and process technology; and

c.

The common basic characteristics.

"Basic scientific research" (GTN NTN) means experimental or theoretical work undertaken principally to acquire new knowledge of the fundamental principles of phenomena or observable facts, not primarily directed towards a specific practical aim or objective.

"Bias" (accelerometer) (7) means the average over a specified time of accelerometer output, measured at specified operating conditions, that has no correlation with input acceleration or rotation. "Bias" is expressed in g or in metres per second squared (g or m/s2). (IEEE Std 528-2001) (Micro g equals 1 × 10-6 g).

"Bias" (gyro) (7) means the average over a specified time of gyro output measured at specified operating conditions that has no correlation with input rotation or acceleration. "Bias" is typically expressed in degrees per hour (deg/hr). (IEEE Std 528-2001).

"Camming" (2) means axial displacement in one revolution of the main spindle measured in a plane perpendicular to the spindle faceplate, at a point next to the circumference of the spindle faceplate (Reference: ISO 230/1 1986, paragraph 5.63).

"Carbon fibre preforms" (1) means an ordered arrangement of uncoated or coated fibres intended to constitute a framework of a part before the "matrix" is introduced to form a "composite".

"CEP" (circle of equal probability) (7) is a measure of accuracy; the radius of the circle centred at the target, at a specific range, in which 50 % of the payloads impact.

"Chemical laser" (6) means a "laser" in which the excited species is produced by the output energy from a chemical reaction.

"Chemical mixture" (1) means a solid, liquid or gaseous product made up of two or more components which do not react together under the conditions under which the mixture is stored.

"Circulation-controlled anti-torque or circulation controlled direction control systems" (7) are systems that use air blown over aerodynamic surfaces to increase or control the forces generated by the surfaces.

"Civil aircraft" (1 3 4 7) means those "aircraft" listed by designation in published airworthiness certification lists by the civil aviation authorities of one or more EU Member States or Wassenaar Arrangement Participating States to fly commercial civil internal and external routes or for legitimate civil, private or business use.

N.B.: See also "aircraft".

"Commingled" (1) means filament to filament blending of thermoplastic fibres and reinforcement fibres in order to produce a fibre reinforcement "matrix" mix in total fibre form.

"Comminution" (1) means a process to reduce a material to particles by crushing or grinding.

"Communications channel controller" (4) means the physical interface which controls the flow of synchronous or asynchronous digital information. It is an assembly that can be integrated into computer or telecommunications equipment to provide communications access.

"Compensation systems" (6) consist of the primary scalar sensor, one or more reference sensors (e.g., vector magnetometers) together with software that permit reduction of rigid body rotation noise of the platform.

"Composite" (1 2 6 8 9) means a "matrix" and an additional phase or additional phases consisting of particles, whiskers, fibres or any combination thereof, present for a specific purpose or purposes.

"Compound rotary table" (2) means a table allowing the workpiece to rotate and tilt about two non-parallel axes, which can be coordinated simultaneously for "contouring control".

"III/V compounds" (3 6) means polycrystalline or binary or complex monocrystalline products consisting of elements of groups IIIA and VA of Mendeleyev's periodic classification table (e.g., gallium arsenide, gallium-aluminium arsenide, indium phosphide).

"Contouring control" (2) means two or more "numerically controlled" motions operating in accordance with instructions that specify the next required position and the required feed rates to that position. These feed rates are varied in relation to each other so that a desired contour is generated (ref. ISO/DIS 2806 - 1980).

"Critical temperature" (1 3 5) (sometimes referred to as the transition temperature) of a specific "superconductive" material means the temperature at which the material loses all resistance to the flow of direct electrical current.

"Cryptographic activation" (5) means any technique that activates or enables cryptographic capability of an item, by means of a secure mechanism implemented by the manufacturer of the item, where this mechanism is uniquely bound to any of the following:

1.

A single instance of the item; or

2.

One customer, for multiple instances of the item.

Technical Notes
1.

"Cryptographic activation" techniques and mechanisms may be implemented as hardware, "software" or "technology".

2.

Mechanisms for "cryptographic activation" can, for example, be serial number-based licence keys or authentication instruments such as digitally signed certificates.

"Cryptography" (5) means the discipline which embodies principles, means and methods for the transformation of data in order to hide its information content, prevent its undetected modification or prevent its unauthorized use. "Cryptography" is limited to the transformation of information using one or more 'secret parameters' (e.g., crypto variables) or associated key management.

Note: "Cryptography" does not include "fixed" data compression or coding techniques.
Technical Note:

'Secret parameter': a constant or key kept from the knowledge of others or shared only within a group.

"CW laser" (6) means a "laser" that produces a nominally constant output energy for greater than 0,25 seconds.

"Data-Based Referenced Navigation" ("DBRN") (7) Systems means systems which use various sources of previously measured geo-mapping data integrated to provide accurate navigation information under dynamic conditions. Data sources include bathymetric maps, stellar maps, gravity maps, magnetic maps or 3-D digital terrain maps.

"Deformable mirrors" (6) (also known as adaptive optic mirrors) means mirrors having:

a.

A single continuous optical reflecting surface which is dynamically deformed by the application of individual torques or forces to compensate for distortions in the optical waveform incident upon the mirror; or

b.

Multiple optical reflecting elements that can be individually and dynamically repositioned by the application of torques or forces to compensate for distortions in the optical waveform incident upon the mirror.

"Depleted uranium" (0) means uranium depleted in the isotope 235 below that occurring in nature.

"Development" (GTN NTN All) is related to all phases prior to serial production, such as: design, design research, design analyses, design concepts, assembly and testing of prototypes, pilot production schemes, design data, process of transforming design data into a product, configuration design, integration design, layouts.

"Diffusion bonding" (1 2 9) means a solid state joining of at least two separate pieces of metals into a single piece with a joint strength equivalent to that of the weakest material, wherein the principal mechanism is interdiffusion of atoms across the interface.

"Digital computer" (4 5) means equipment which can, in the form of one or more discrete variables, perform all of the following:

a.

Accept data;

b.

Store data or instructions in fixed or alterable (writable) storage devices;

c.

Process data by means of a stored sequence of instructions which is modifiable; and

d.

Provide output of data.

N.B.: Modifications of a stored sequence of instructions include replacement of fixed storage devices, but not a physical change in wiring or interconnections.

"Digital transfer rate" (def) means the total bit rate of the information that is directly transferred on any type of medium.

N.B.: See also "total digital transfer rate".

"Direct-acting hydraulic pressing" (2) means a deformation process which uses a fluid-filled flexible bladder in direct contact with the workpiece.

"Drift rate" (gyro) (7) means the component of gyro output that is functionally independent of input rotation. It is expressed as an angular rate. (IEEE STD 528-2001).

"Effective gramme" (0 1) of "special fissile material" means:

a.

For plutonium isotopes and uranium-233, the isotope weight in grammes;

b.

For uranium enriched 1 per cent or greater in the isotope uranium-235, the element weight in grammes multiplied by the square of its enrichment expressed as a decimal weight fraction;

c.

For uranium enriched below 1 per cent in the isotope uranium-235, the element weight in grammes multiplied by 0,0001;

"Electronic assembly" (2 3 4 5) means a number of electronic components (i.e., 'circuit elements', 'discrete components', integrated circuits, etc.) connected together to perform (a) specific function(s), replaceable as an entity and normally capable of being disassembled.

N.B. 1: 'Circuit element': a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.
N.B. 2: 'Discrete component': a separately packaged 'circuit element' with its own external connections.

"Electronically steerable phased array antenna" (5 6) means an antenna which forms a beam by means of phase coupling, i.e., the beam direction is controlled by the complex excitation coefficients of the radiating elements and the direction of that beam can be varied in azimuth or in elevation, or both, by application, both in transmission and reception, of an electrical signal.

"Energetic materials" (1) means substances or mixtures that react chemically to release energy required for their intended application. "Explosives", "pyrotechnics" and "propellants" are subclasses of energetic materials.

"End-effectors" (2) means grippers, 'active tooling units' and any other tooling that is attached to the baseplate on the end of a "robot" manipulator arm.

N.B.: 'Active tooling unit' means a device for applying motive power, process energy or sensing to the workpiece.

"Equivalent Density" (6) means the mass of an optic per unit optical area projected onto the optical surface.

"Explosives" (1) means solid, liquid or gaseous substances or mixtures of substances which, in their application as primary, booster, or main charges in warheads, demolition and other applications, are required to detonate.

"FADEC Systems" (7 9) means Full Authority Digital Engine Control Systems – A digital electronic control system for a gas turbine engine that is able to autonomously control the engine throughout its whole operating range from demanded engine start until demanded engine shut-down, in both normal and fault conditions.

"Fibrous or filamentary materials" (0 1 8) include:

a.

Continuous "monofilaments";

b.

Continuous "yarns" and "rovings";

c.

"Tapes", fabrics, random mats and braids;

d.

Chopped fibres, staple fibres and coherent fibre blankets;

e.

Whiskers, either monocrystalline or polycrystalline, of any length;

f.

Aromatic polyamide pulp.

"Film type integrated circuit" (3) means an array of 'circuit elements' and metallic interconnections formed by deposition of a thick or thin film on an insulating "substrate".

N.B.: 'Circuit element' is a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

"Fixed" (5) means that the coding or compression algorithm cannot accept externally supplied parameters (e.g., cryptographic or key variables) and cannot be modified by the user.

"Flight control optical sensor array" (7) is a network of distributed optical sensors, using "laser" beams, to provide real-time flight control data for on-board processing.

"Flight path optimisation" (7) is a procedure that minimizes deviations from a four-dimensional (space and time) desired trajectory based on maximizing performance or effectiveness for mission tasks.

"Fly-by-light system" (7) means a primary digital flight control system employing feedback to control the aircraft during flight, where the commands to the effectors/actuators are optical signals.

"Fly-by-wire system" (7) means a primary digital flight control system employing feedback to control the aircraft during flight, where the commands to the effectors/actuators are electrical signals.

"Focal plane array" (6 8) means a linear or two-dimensional planar layer, or combination of planar layers, of individual detector elements, with or without readout electronics, which work in the focal plane.

N.B.: This is not intended to include a stack of single detector elements or any two, three or four element detectors provided time delay and integration is not performed within the element.

"Fractional bandwidth" (3 5) means the "instantaneous bandwidth" divided by the centre frequency, expressed as a percentage.

"Frequency hopping" (5) means a form of "spread spectrum" in which the transmission frequency of a single communication channel is made to change by a random or pseudo-random sequence of discrete steps.

"Frequency mask trigger" (3) for "signal analysers" is a mechanism where the trigger function is able to select a frequency range to be triggered on as a subset of the acquisition bandwidth while ignoring other signals that may also be present within the same acquisition bandwidth. A "frequency mask trigger" may contain more than one independent set of limits.

"Frequency switching time" (3) means the time (i.e., delay) taken by a signal when switched from an initial specified output frequency, to arrive at or within ± 0,05 % of a final specified output frequency. Items having a specified frequency range of less than ± 0,05 % around their centre frequency are defined to be incapable of frequency switching.

"Frequency synthesiser" (3) means any kind of frequency source, regardless of the actual technique used, providing a multiplicity of simultaneous or alternative output frequencies, from one or more outputs, controlled by, derived from or disciplined by a lesser number of standard (or master) frequencies.

"Fuel cell" (8) is an electrochemical device that converts chemical energy directly into Direct Current (DC) electricity by consuming fuel from an external source.

"Fusible" (1) means capable of being cross-linked or polymerized further (cured) by the use of heat, radiation, catalysts, etc., or that can be melted without pyrolysis (charring).

"Gas Atomisation" (1) means a process to reduce a molten stream of metal alloy to droplets of 500 micrometre diameter or less by a high pressure gas stream.

"Geographically dispersed" (6) is where each location is distant from any other more than 1 500 m in any direction. Mobile sensors are always considered "geographically dispersed".

"Guidance set" (7) means systems that integrate the process of measuring and computing a vehicles position and velocity (i.e. navigation) with that of computing and sending commands to the vehicles flight control systems to correct the trajectory.

"Hot isostatic densification" (2) means the process of pressurising a casting at temperatures exceeding 375 K (102 °C) in a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal force in all directions to reduce or eliminate internal voids in the casting.

"Hybrid integrated circuit" (3) means any combination of integrated circuit(s), or integrated circuit with 'circuit elements' or 'discrete components' connected together to perform (a) specific function(s), and having all of the following characteristics:

a.

Containing at least one unencapsulated device;

b.

Connected together using typical IC production methods;

c.

Replaceable as an entity; and

d.

Not normally capable of being disassembled.

N.B. 1: 'Circuit element': a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.
N.B. 2: 'Discrete component': a separately packaged 'circuit element' with its own external connections.

"Image enhancement" (4) means the processing of externally derived information-bearing images by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform). This does not include algorithms using only linear or rotational transformation of a single image, such as translation, feature extraction, registration or false coloration.

"Immunotoxin" (1) is a conjugate of one cell specific monoclonal antibody and a "toxin" or "sub-unit of toxin", that selectively affects diseased cells.

"In the public domain" (GTN NTN GSN), as it applies herein, means "technology" or "software" which has been made available without restrictions upon its further dissemination (copyright restrictions do not remove "technology" or "software" from being "in the public domain").

"Information security" (4 5) is all the means and functions ensuring the accessibility, confidentiality or integrity of information or communications, excluding the means and functions intended to safeguard against malfunctions. This includes "cryptography", "cryptographic activation", 'cryptanalysis', protection against compromising emanations and computer security.

N.B.: 'Cryptanalysis': analysis of a cryptographic system or its inputs and outputs to derive confidential variables or sensitive data, including clear text.

"Instantaneous bandwidth" (3 5 7) means the bandwidth over which output power remains constant within 3 dB without adjustment of other operating parameters.

"Instrumented range" (6) means the specified unambiguous display range of a radar.

"Insulation" (9) is applied to the components of a rocket motor, i.e. the case, nozzle, inlets, case closures, and includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.

"Interior lining" (9) is suited for the bond interface between the solid propellant and the case or insulating liner. Usually a liquid polymer based dispersion of refractory or insulating materials, e.g. carbon filled hydroxyl terminated polybutadiene (HTPB) or other polymer with added curing agents sprayed or screeded over a case interior.

"Intrinsic Magnetic Gradiometer" (6) is a single magnetic field gradient sensing element and associated electronics the output of which is a measure of magnetic field gradient.

N.B.: See also "magnetic gradiometer".

"Intrusion software" (4) means "software" specially designed or modified to avoid detection by 'monitoring tools', or to defeat 'protective countermeasures', of a computer or network-capable device, and performing any of the following:

a.

The extraction of data or information, from a computer or network-capable device, or the modification of system or user data; or

b.

The modification of the standard execution path of a program or process in order to allow the execution of externally provided instructions.

Notes:
1.

"Intrusion software" does not include any of the following:

a.

Hypervisors, debuggers or Software Reverse Engineering (SRE) tools;

b.

Digital Rights Management (DRM) "software"; or

c.

"Software" designed to be installed by manufacturers, administrators or users, for the purposes of asset tracking or recovery.

2.

Network-capable devices include mobile devices and smart meters.

Technical Notes:
1.

'Monitoring tools': "software" or hardware devices, that monitor system behaviours or processes running on a device. This includes antivirus (AV) products, end point security products, Personal Security Products (PSP), Intrusion Detection Systems (IDS), Intrusion Prevention Systems (IPS) or firewalls.

2.

'Protective countermeasures': techniques designed to ensure the safe execution of code, such as Data Execution Prevention (DEP), Address Space Layout Randomisation (ASLR) or sandboxing.

"Isolated live cultures" (1) includes live cultures in dormant form and in dried preparations.

"Isostatic presses" (2) mean equipment capable of pressurising a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a workpiece or material.

"Laser" (0 2 3 5 6 7 8 9) is an assembly of components which produce both spatially and temporally coherent light that is amplified by stimulated emission of radiation.

N.B.: See also

"Chemical laser"

"Super High Power Laser";

"Transfer laser".

"Library" (1) (parametric technical database) means a collection of technical information, reference to which may enhance the performance of relevant systems, equipment or components.

"Lighter-than-air vehicles" (9) means balloons and airships that rely on hot air or other lighter-than-air gases such as helium or hydrogen for their lift.

"Linearity" (2) (usually measured in terms of non-linearity) means the maximum deviation of the actual characteristic (average of upscale and downscale readings), positive or negative, from a straight line so positioned as to equalise and minimise the maximum deviations.

"Local area network" (4 5) is a data communication system having all of the following characteristics:

a.

Allows an arbitrary number of independent 'data devices' to communicate directly with each other; and

b.

Is confined to a geographical area of moderate size (e.g., office building, plant, campus, warehouse).

N.B.: 'Data device' means equipment capable of transmitting or receiving sequences of digital information.

"Magnetic Gradiometers" (6) are instruments designed to detect the spatial variation of magnetic fields from sources external to the instrument. They consist of multiple "magnetometers" and associated electronics the output of which is a measure of magnetic field gradient.

N.B. See also "intrinsic magnetic gradiometer".

"Magnetometers" (6) are instruments designed to detect magnetic fields from sources external to the instrument. They consist of a single magnetic field sensing element and associated electronics the output of which is a measure of the magnetic field.

"Main storage" (4) means the primary storage for data or instructions for rapid access by a central processing unit. It consists of the internal storage of a "digital computer" and any hierarchical extension thereto, such as cache storage or non-sequentially accessed extended storage.

"Materials resistant to corrosion by UF6" (0) include copper, copper alloys, stainless steel, aluminium, aluminium oxide, aluminium alloys, nickel or alloys containing 60 % or more nickel by weight and fluorinated hydrocarbon polymers.

"Matrix" (1 2 8 9) means a substantially continuous phase that fills the space between particles, whiskers or fibres.

"Measurement uncertainty" (2) is the characteristic parameter which specifies in what range around the output value the correct value of the measurable variable lies with a confidence level of 95 %. It includes the uncorrected systematic deviations, the uncorrected backlash and the random deviations (ref. ISO 10360-2).

"Mechanical Alloying" (1) means an alloying process resulting from the bonding, fracturing and rebonding of elemental and master alloy powders by mechanical impact. Non-metallic particles may be incorporated in the alloy by addition of the appropriate powders.

"Melt Extraction" (1) means a process to 'solidify rapidly' and extract a ribbon-like alloy product by the insertion of a short segment of a rotating chilled block into a bath of a molten metal alloy.

N.B.: 'Solidify rapidly': solidification of molten material at cooling rates exceeding 1 000 K/s.

"Melt Spinning" (1) means a process to 'solidify rapidly' a molten metal stream impinging upon a rotating chilled block, forming a flake, ribbon or rod-like product.

N.B.: 'Solidify rapidly': solidification of molten material at cooling rates exceeding 1 000 K/s.

"Microcomputer microcircuit" (3) means a "monolithic integrated circuit" or "multichip integrated circuit" containing an arithmetic logic unit (ALU) capable of executing general purpose instructions from an internal storage, on data contained in the internal storage.

N.B.: The internal storage may be augmented by an external storage.

"Microprocessor microcircuit" (3) means a "monolithic integrated circuit" or "multichip integrated circuit" containing an arithmetic logic unit (ALU) capable of executing a series of general purpose instructions from an external storage.

N.B. 1: The "microprocessor microcircuit" normally does not contain integral user-accessible storage, although storage present on-the-chip may be used in performing its logic function.
N.B. 2: This includes chip sets which are designed to operate together to provide the function of a "microprocessor microcircuit".

"Microorganisms" (1 2) means bacteria, viruses, mycoplasms, rickettsiae, chlamydiae or fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures.

"Missiles" (1 3 6 7 9) means complete rocket systems and unmanned aerial vehicle systems, capable of delivering at least 500 kg payload to a range of at least 300 km.

"Monofilament" (1) or filament is the smallest increment of fibre, usually several micrometres in diameter.

"Monolithic integrated circuit" (3) means a combination of passive or active 'circuit elements' or both which:

a.

Are formed by means of diffusion processes, implantation processes or deposition processes in or on a single semiconducting piece of material, a so-called 'chip';

b.

Can be considered as indivisibly associated; and

c.

Perform the function(s) of a circuit.

N.B.: 'Circuit element' is a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

"Monospectral imaging sensors" (6) are capable of acquisition of imaging data from one discrete spectral band.

"Multichip integrated circuit" (3) means two or more "monolithic integrated circuits" bonded to a common "substrate".

"Multispectral imaging sensors" (6) are capable of simultaneous or serial acquisition of imaging data from two or more discrete spectral bands. Sensors having more than twenty discrete spectral bands are sometimes referred to as hyperspectral imaging sensors.

"Natural uranium" (0) means uranium containing the mixtures of isotopes occurring in nature.

"Network access controller" (4) means a physical interface to a distributed switching network. It uses a common medium which operates throughout at the same "digital transfer rate" using arbitration (e.g., token or carrier sense) for transmission. Independently from any other, it selects data packets or data groups (e.g., IEEE 802) addressed to it. It is an assembly that can be integrated into computer or telecommunications equipment to provide communications access.

"Neural computer" (4) means a computational device designed or modified to mimic the behaviour of a neuron or a collection of neurons, i.e., a computational device which is distinguished by its hardware capability to modulate the weights and numbers of the interconnections of a multiplicity of computational components based on previous data.

"Nuclear reactor" (0) means a complete reactor capable of operation so as to maintain a controlled self-sustaining fission chain reaction. A "nuclear reactor" includes all the items within or attached directly to the reactor vessel, the equipment which controls the level of power in the core, and the components which normally contain, come into direct contact with or control the primary coolant of the reactor core.

"Numerical control" (2) means the automatic control of a process performed by a device that makes use of numeric data usually introduced as the operation is in progress (ref. ISO 2382).

"Object code" (GSN) means an equipment executable form of a convenient expression of one or more processes ("source code" (source language)) which has been compiled by programming system.

"Operations, Administration or Maintenance" ("OAM") (5) means performing one or more of the following tasks:

a.

Establishing or managing any of the following:

1.

Accounts or privileges of users or administrators;

2.

Settings of an item; or

3.

Authentication data in support of the tasks described in paragraphs a.1. or a.2.;

b.

Monitoring or managing the operating condition or performance of an item; or

c.

Managing logs or audit data in support of any of the tasks described in paragraphs a. or b.

Note: "OAM" does not include any of the following tasks or their associated key management functions:
a.

Provisioning or upgrading any cryptographic functionality that is not directly related to establishing or managing authentication data in support of the tasks described in paragraphs a.1. or a.2. above; or

b.

Performing any cryptographic functionality on the forwarding or data plane of an item.

"Optical amplification" (5), in optical communications, means an amplification technique that introduces a gain of optical signals that have been generated by a separate optical source, without conversion to electrical signals, i.e., using semiconductor optical amplifiers, optical fibre luminescent amplifiers.

"Optical computer" (4) means a computer designed or modified to use light to represent data and whose computational logic elements are based on directly coupled optical devices.

"Optical integrated circuit" (3) means a "monolithic integrated circuit" or a "hybrid integrated circuit", containing one or more parts designed to function as a photosensor or photoemitter or to perform (an) optical or (an) electro-optical function(s).

"Optical switching" (5) means the routing of or switching of signals in optical form without conversion to electrical signals.

"Overall current density" (3) means the total number of ampere-turns in the coil (i.e., the sum of the number of turns multiplied by the maximum current carried by each turn) divided by the total cross-section of the coil (comprising the superconducting filaments, the metallic matrix in which the superconducting filaments are embedded, the encapsulating material, any cooling channels, etc.).

"Participating state" (7 9) is a state participating in the Wassenaar Arrangement (see www.wassenaar.org

"Peak power" (6) means the highest power attained in the "pulse duration".

"Personal area network" (5) means a data communication system having all of the following characteristics:

a.

Allows an arbitrary number of independent or interconnected 'data devices' to communicate directly with each other; and

b.

Is confined to the communication between devices within the immediate vicinity of an individual person or device controller (e.g., single room, office, or automobile, and their nearby surrounding spaces).

Technical Note:

'Data device' means equipment capable of transmitting or receiving sequences of digital information.

"Plasma atomisation" (1) means a process to reduce a molten stream or solid metal to droplets of 500 μm diameter or less, using plasma torches in an inert gas environment.

"Power management" (7) means changing the transmitted power of the altimeter signal so that received power at the "aircraft" altitude is always at the minimum necessary to determine the altitude.

"Previously separated" (0 1) means the application of any process intended to increase the concentration of the controlled isotope.

"Primary flight control" (7) means an "aircraft" stability or manoeuvering control using force/moment generators, i.e., aerodynamic control surfaces or propulsive thrust vectoring.

"Principal element" (4), as it applies in Category 4, is a "principal element" when its replacement value is more than 35 % of the total value of the system of which it is an element. Element value is the price paid for the element by the manufacturer of the system, or by the system integrator. Total value is the normal international selling price to unrelated parties at the point of manufacture or consolidation of shipment.

"Production" (GTN NTN All) means all production phases, such as: construction, production engineering, manufacture, integration, assembly (mounting), inspection, testing, quality assurance.

"Production equipment" (1 7 9) means tooling, templates, jigs, mandrels, moulds, dies, fixtures, alignment mechanisms, test equipment, other machinery and components therefor, limited to those specially designed or modified for "development" or for one or more phases of "production".

"Production facilities" (7 9) means "production equipment" and specially designed software therefor integrated into installations for "development" or for one or more phases of "production".

"Programme" (2 6) means a sequence of instructions to carry out a process in, or convertible into, a form executable by an electronic computer.

"Pulse compression" (6) means the coding and processing of a radar signal pulse of long time duration to one of short time duration, while maintaining the benefits of high pulse energy.

"Pulse duration" (6) is the duration of a "laser" pulse and means the time between the half-power points on the leading edge and trailing edge of an individual pulse.

"Pulsed laser" (6) means a "laser" having a "pulse duration" that is less than or equal to 0,25 seconds.

"Quantum cryptography" (5) means a family of techniques for the establishment of shared key for "cryptography" by measuring the quantum-mechanical properties of a physical system (including those physical properties explicitly governed by quantum optics, quantum field theory or quantum electrodynamics).

"Radar frequency agility" (6) means any technique which changes, in a pseudo-random sequence, the carrier frequency of a pulsed radar transmitter between pulses or between groups of pulses by an amount equal to or larger than the pulse bandwidth.

"Radar spread spectrum" (6) means any modulation technique for spreading energy originating from a signal with a relatively narrow frequency band, over a much wider band of frequencies, by using random or pseudo-random coding.

"Radiant sensitivity" (6) is Radiant sensitivity (mA/W) = 0,807 × (wavelength in nm) × Quantum Efficiency (QE).

Technical Note:

QE is usually expressed as a percentage; however, for the purposes of this formula QE is expressed as a decimal number less than one, e.g., 78 % is 0,78.

"Real-time bandwidth" (3) for "signal analysers" is the widest frequency range for which the analyser can continuously transform time-domain data entirely into frequency-domain results, using a Fourier or other discrete time transformation that processes every incoming time point without gaps or windowing effects that causes a reduction of measured amplitude of more than 3 dB below the actual signal amplitude, while outputting or displaying the transformed data.

"Real time processing" (2 6 7) means the processing of data by a computer system providing a required level of service, as a function of available resources, within a guaranteed response time, regardless of the load of the system, when stimulated by an external event.

"Repeatability" (7) means the closeness of agreement among repeated measurements of the same variable under the same operating conditions when changes in conditions or non-operating periods occur between measurements. (Reference: IEEE STD 528-2001 (one sigma standard deviation))

"Required" (GTN 1-9), as applied to "technology", refers to only that portion of "technology" which is peculiarly responsible for achieving or extending the controlled performance levels, characteristics or functions. Such "required" "technology" may be shared by different goods.

"Resolution" (2) means the least increment of a measuring device; on digital instruments, the least significant bit (ref. ANSI B-89.1.12).

"Riot control agent" (1) means substances which, under the expected conditions of use for riot control purposes, produce rapidly in humans sensory irritation or disabling physical effects which disappear within a short time following termination of exposure.

Technical Note:

Tear gases are a subset of "riot control agents".

"Robot" (2 8) means a manipulation mechanism, which may be of the continuous path or of the point-to-point variety, may use sensors, and has all the following characteristics:

a.

Is multifunctional;

b.

Is capable of positioning or orienting material, parts, tools or special devices through variable movements in three dimensional space;

c.

Incorporates three or more closed or open loop servo-devices which may include stepping motors; and

d.

Has "user accessible programmability" by means of teach/playback method or by means of an electronic computer which may be a programmable logic controller, i.e., without mechanical intervention.

N.B.: The above definition does not include the following devices:
1.

Manipulation mechanisms which are only manually/ teleoperator controllable;

2.

Fixed sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions. The programme is mechanically limited by fixed stops, such as pins or cams. The sequence of motions and the selection of paths or angles are not variable or changeable by mechanical, electronic or electrical means;

3.

Mechanically controlled variable sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions. The programme is mechanically limited by fixed, but adjustable stops, such as pins or cams. The sequence of motions and the selection of paths or angles are variable within the fixed programme pattern. Variations or modifications of the programme pattern (e.g., changes of pins or exchanges of cams) in one or more motion axes are accomplished only through mechanical operations;

4.

Non-servo-controlled variable sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions. The programme is variable but the sequence proceeds only by the binary signal from mechanically fixed electrical binary devices or adjustable stops;

5.

Stacker cranes defined as Cartesian coordinate manipulator systems manufactured as an integral part of a vertical array of storage bins and designed to access the contents of those bins for storage or retrieval.

"Rotary atomisation" (1) means a process to reduce a stream or pool of molten metal to droplets to a diameter of 500 micrometre or less by centrifugal force.

"Roving" (1) is a bundle (typically 12-120) of approximately parallel 'strands'.

N.B.: 'Strand' is a bundle of "monofilaments" (typically over 200) arranged approximately parallel.

"Run-out" (2) (out-of-true running) means radial displacement in one revolution of the main spindle measured in a plane perpendicular to the spindle axis at a point on the external or internal revolving surface to be tested (Reference: ISO 230/1 1986, paragraph 5.61).

"Scale factor" (gyro or accelerometer) (7) means the ratio of change in output to a change in the input intended to be measured. Scale factor is generally evaluated as the slope of the straight line that can be fitted by the method of least squares to input-output data obtained by varying the input cyclically over the input range.

"Settling time" (3) means the time required for the output to come within one-half bit of the final value when switching between any two levels of the converter.

"SHPL" is equivalent to "super high power laser".

"Signal analysers" (3) means apparatus capable of measuring and displaying basic properties of the single-frequency components of multi-frequency signals.

"Signal processing" (3 4 5 6) means the processing of externally derived information-bearing signals by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform).

"Software" (GSN All) means a collection of one or more "programmes" or 'microprogrammes' fixed in any tangible medium of expression.

N.B.: 'Microprogramme' means a sequence of elementary instructions, maintained in a special storage, the execution of which is initiated by the introduction of its reference instruction into an instruction register.

"Source code" (or source language) (6 7 9) is a convenient expression of one or more processes which may be turned by a programming system into equipment executable form ("object code" (or object language)).

"Spacecraft" (7 9) means active and passive satellites and space probes.

"Spacecraft bus" (9) means equipment that provides the support infrastructure of the "spacecraft" and location for the "spacecraft payload".

"Spacecraft payload" (9) means equipment, attached to the "spacecraft bus", designed to perform a mission in space (e.g., communications, observation, science).

"Space-qualified" (3 6 7) means designed, manufactured or qualified through successful testing, for operation at altitudes greater than 100 km above the surface of the Earth.

N.B.: A determination that a specific item is "Space-qualified" by virtue of testing does not mean that other items in the same production run or model series are "Space-qualified" if not individually tested.

"Special fissile material" (0) means plutonium-239, uranium-233, "uranium enriched in the isotopes 235 or 233", and any material containing the foregoing.

"Specific modulus" (0 1 9) is Young's modulus in pascals, equivalent to N/m2 divided by specific weight in N/m3, measured at a temperature of (296 ± 2) K ((23 ± 2) °C) and a relative humidity of (50 ± 5) %.

"Specific tensile strength" (0 1 9) is ultimate tensile strength in pascals, equivalent to N/m2 divided by specific weight in N/m3, measured at a temperature of (296 ± 2) K ((23 ± 2) °C) and a relative humidity of (50 ± 5) %.

"Spinning mass gyros" (7) means gyros which use a continually rotating mass to sense angular motion.

"Splat Quenching" (1) means a process to 'solidify rapidly' a molten metal stream impinging upon a chilled block, forming a flake-like product.

N.B.: 'Solidify rapidly' solidification of molten material at cooling rates exceeding 1 000 K/s.

"Spread spectrum" (5) means the technique whereby energy in a relatively narrow-band communication channel is spread over a much wider energy spectrum.

"Spread spectrum" radar (6) - see "Radar spread spectrum".

"Stability" (7) means the standard deviation (1 sigma) of the variation of a particular parameter from its calibrated value measured under stable temperature conditions. This can be expressed as a function of time.

"States (not) Party to the Chemical Weapon Convention" (1) are those states for which the Convention on the Prohibition of the Development, Production, Stockpiling and Use of Chemical Weapons has (not) entered into force. (See www.opcw.org)

"Substrate" (3) means a sheet of base material with or without an interconnection pattern and on which or within which 'discrete components' or integrated circuits or both can be located.

N.B. 1: 'Discrete component': a separately packaged 'circuit element' with its own external connections.
N.B. 2: 'Circuit element': a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

"Substrate blanks" (3 6) means monolithic compounds with dimensions suitable for the production of optical elements such as mirrors or optical windows.

"Sub-unit of toxin" (1) is a structurally and functionally discrete component of a whole "toxin".

"Superalloys" (2 9) means nickel-, cobalt- or iron-base alloys having strengths superior to any alloys in the AISI 300 series at temperatures over 922 K (649 °C) under severe environmental and operating conditions.

"Superconductive" (1 3 5 6 8) means materials, i.e., metals, alloys or compounds, which can lose all electrical resistance, i.e., which can attain infinite electrical conductivity and carry very large electrical currents without Joule heating.

N.B.: The "superconductive" state of a material is individually characterised by a "critical temperature", a critical magnetic field, which is a function of temperature, and a critical current density which is, however, a function of both magnetic field and temperature.

"Super High Power Laser" ("SHPL") (6) means a "laser" capable of delivering (the total or any portion of) the output energy exceeding 1 kJ within 50 ms or having an average or CW power exceeding 20 kW.

"Superplastic forming" (1 2) means a deformation process using heat for metals that are normally characterised by low values of elongation (less than 20 %) at the breaking point as determined at room temperature by conventional tensile strength testing, in order to achieve elongations during processing which are at least 2 times those values.

"Symmetric algorithm" (5) means a cryptographic algorithm using an identical key for both encryption and decryption.

N.B.: A common use of "symmetric algorithms" is confidentiality of data.

"System tracks" (6) means processed, correlated (fusion of radar target data to flight plan position) and updated aircraft flight position report available to the Air Traffic Control centre controllers.

"Systolic array computer" (4) means a computer where the flow and modification of the data is dynamically controllable at the logic gate level by the user.

"Tape" (1) is a material constructed of interlaced or unidirectional "monofilaments", 'strands', "rovings", "tows", or "yarns", etc., usually pre-impregnated with resin.

N.B.: 'Strand' is a bundle of "monofilaments" (typically over 200) arranged approximately parallel.

"Technology" (GTN NTN All) means specific information necessary for the "development", "production" or "use" of goods. This information takes the form of 'technical data' or 'technical assistance'.

N.B. 1: 'Technical assistance' may take forms such as instructions, skills, training, working knowledge and consulting services and may involve the transfer of 'technical data'.
N.B. 2: 'Technical data' may take forms such as blueprints, plans, diagrams, models, formulae, tables, engineering designs and specifications, manuals and instructions written or recorded on other media or devices such as disk, tape, read-only memories.

"Three dimensional integrated circuit" (3) means a collection of semiconductor die, integrated together, and having vias passing completely through at least one die to establish interconnections between die.

"Tilting spindle" (2) means a tool-holding spindle which alters, during the machining process, the angular position of its centre line with respect to any other axis.

"Time constant" (6) is the time taken from the application of a light stimulus for the current increment to reach a value of 1-1/e times the final value (i.e., 63 % of the final value).

"Tip shroud" (9) means a stationary ring component (solid or segmented) attached to the inner surface of the engine turbine casing or a feature at the outer tip of the turbine blade, which primarily provides a gas seal between the stationary and rotating components.

"Total control of flight" (7) means an automated control of "aircraft" state variables and flight path to meet mission objectives responding to real time changes in data regarding objectives, hazards or other "aircraft".

"Total digital transfer rate" (5) means the number of bits, including line coding, overhead and so forth per unit time passing between corresponding equipment in a digital transmission system.

N.B.: See also "digital transfer rate".

"Tow" (1) is a bundle of "monofilaments", usually approximately parallel.

"Toxins" (1 2) means toxins in the form of deliberately isolated preparations or mixtures, no matter how produced, other than toxins present as contaminants of other materials such as pathological specimens, crops, foodstuffs or seed stocks of "microorganisms".

"Transfer laser" (6) means a "laser" in which the lasing species is excited through the transfer of energy by collision of a non-lasing atom or molecule with a lasing atom or molecule species.

"Tunable" (6) means the ability of a "laser" to produce a continuous output at all wavelengths over a range of several "laser" transitions. A line selectable "laser" produces discrete wavelengths within one "laser" transition and is not considered "tunable".

"Unidirectional positioning repeatability" (2) means the smaller of values R↑ and R↓ (forward and backward), as defined by 3.21 of ISO 230-2:2014 or national equivalents, of an individual machine tool axis.

"Unmanned Aerial Vehicle" ("UAV") (9) means any aircraft capable of initiating flight and sustaining controlled flight and navigation without any human presence on board.

"Uranium enriched in the isotopes 235 or 233" (0) means uranium containing the isotopes 235 or 233, or both, in an amount such that the abundance ratio of the sum of these isotopes to the isotope 238 is more than the ratio of the isotope 235 to the isotope 238 occurring in nature (isotopic ratio 0,71 per cent).

"Use" (GTN NTN All) means operation, installation (including on-site installation), maintenance (checking), repair, overhaul and refurbishing.

"User accessible programmability" (6) means the facility allowing a user to insert, modify or replace "programmes" by means other than:

a.

A physical change in wiring or interconnections; or

b.

The setting of function controls including entry of parameters.

"Vaccine" (1) is a medicinal product in a pharmaceutical formulation licensed by, or having marketing or clinical trial authorisation from, the regulatory authorities of either the country of manufacture or of use, which is intended to stimulate a protective immunological response in humans or animals in order to prevent disease in those to whom or to which it is administered.

"Vacuum Atomisation" (1) means a process to reduce a molten stream of metal to droplets of a diameter of 500 micrometre or less by the rapid evolution of a dissolved gas upon exposure to a vacuum.

"Variable geometry airfoils" (7) means the use of trailing edge flaps or tabs, or leading edge slats or pivoted nose droop, the position of which can be controlled in flight.

"Yarn" (1) is a bundle of twisted 'strands'.

N.B.: 'Strand' is a bundle of "monofilaments" (typically over 200) arranged approximately parallel.
CATEGORY 0 — NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT
[0A] Systems, Equipment and Components

[0A001] "Nuclear reactors" and specially designed or prepared equipment and components therefor, as follows:

a.

"Nuclear reactors";

b.

Metal vessels, or major shop-fabricated parts therefor, including the reactor vessel head for a reactor pressure vessel, specially designed or prepared to contain the core of a "nuclear reactor";

c.

Manipulative equipment specially designed or prepared for inserting or removing fuel in a "nuclear reactor";

d.

Control rods specially designed or prepared for the control of the fission process in a "nuclear reactor", support or suspension structures therefor, rod drive mechanisms and rod guide tubes;

e.

Pressure tubes specially designed or prepared to contain both fuel elements and the primary coolant in a "nuclear reactor";

f.

Zirconium metal tubes or zirconium alloy tubes (or assembles of tubes) specially designed or prepared for use as fuel cladding in a "nuclear reactor", and in quantities exceeding 10 kg;

'Nuclear reactor internals' specially designed or prepared for use in a "nuclear reactor", including support columns for the core, fuel channels, calandria tubes, thermal shields, baffles, core grid plates, and diffuser plates;

[0B] Test, Inspection and Production Equipment

[0B001] Plant for the separation of isotopes of "natural uranium", "depleted uranium" or "special fissile materials", and specially designed or prepared equipment and components therefor, as follows:

a.

Plant specially designed for separating isotopes of "natural uranium", "depleted uranium", and "special fissile materials", as follows:

1.

Gas centrifuge separation plant;

2.

Gaseous diffusion separation plant;

3.

Aerodynamic separation plant;

4.

Chemical exchange separation plant;

5.

Ion-exchange separation plant;

6.

Atomic vapour "laser" isotope separation plant;

7.

Molecular "laser" isotope separation plant;

8.

Plasma separation plant;

9.

Electro magnetic separation plant;

b.

Gas centrifuges and assemblies and components, specially designed or prepared for gas centrifuge separation process, as follows:

Technical Note:

In 0B001.b. 'high strength-to-density ratio material' means any of the following:

1.

Maraging steel capable of an ultimate tensile strength of 1,95 GPa or more;

2.

Aluminium alloys capable of an ultimate tensile strength of 0,46 GPa or more; or

3.

"Fibrous or filamentary materials" with a "specific modulus" of more than 3,18 × 106 m and a "specific tensile strength" greater than 7,62 × 104 m;

1.

Gas centrifuges;

2.

Complete rotor assemblies;

3.

Rotor tube cylinders with a wall thickness of 12 mm or less, a diameter of between 75 mm and 650 mm, made from 'high strength-to-density ratio materials';

4.

Rings or bellows with a wall thickness of 3 mm or less and a diameter of between 75 mm and 650 mm and designed to give local support to a rotor tube or to join a number together, made from 'high strength-to-density ratio materials';

5.

Baffles of between 75 mm and 650 mm diameter for mounting inside a rotor tube, made from 'high strength-to-density ratio materials'.

6.

Top or bottom caps of between 75 mm and 650 mm diameter to fit the ends of a rotor tube, made from 'high strength-to-density ratio materials';

7.

Magnetic suspension bearings as follows:

a.

Bearing assemblies consisting of an annular magnet suspended within a housing made of or protected by "materials resistant to corrosion by UF6" containing a damping medium and having the magnet coupling with a pole piece or second magnet fitted to the top cap of the rotor;

b.

Active magnetic bearings specially designed or prepared for use with gas centrifuges.

8.

Specially prepared bearings comprising a pivot-cup assembly mounted on a damper;

9.

Molecular pumps comprised of cylinders having internally machined or extruded helical grooves and internally machined bores;

10.

Ring-shaped motor stators for multiphase AC hysteresis (or reluctance) motors for synchronous operation within a vacuum at a frequency of 600 Hz or more and a power of 40 VA or more;

11.

Centrifuge housing/recipients to contain the rotor tube assembly of a gas centrifuge, consisting of a rigid cylinder of wall thickness up to 30 mm with precision machined ends that are parallel to each other and perpendicular to the cylinder's longitudinal axis to within 0,05 degrees or less;

12.

Scoops consisting of specially designed or prepared tubes for the extraction of UF6 gas from within the rotor tube by a Pitot tube action and capable of being fixed to the central gas extraction system;

13.

Frequency changers (converters or inverters) specially designed or prepared to supply motor stators for gas centrifuge enrichment, having all of the following characteristics, and specially designed components therefor:

a.

A multiphase frequency output of 600 Hz or greater; and

b.

High stability (with frequency control better than 0,2 %);

14.

Shut-off and control valves as follows:

a.

Shut-off valves specially designed or prepared to act on the feed, product or tails UF6 gaseous streams of an individual gas centrifuge;

b.

Bellows-sealed valves, shut-off or control, made of or protected by "materials resistant to corrosion by UF6", with an inside diameter of 10 mm to 160 mm, specially designed or prepared for use in main or auxiliary systems of gas centrifuge enrichment plants;

Equipment and components, specially designed or prepared for laser-based separation processes using atomic vapour laser isotope separation, as follows:

Equipment and components, specially designed or prepared for laser-based separation processes using molecular laser isotope separation, as follows:

[0B002] Specially designed or prepared auxiliary systems, equipment and components as follows, for isotope separation plant specified in 0B001, made of or protected by "materials resistant to corrosion by UF6":

a.

Feed autoclaves, ovens or systems used for passing UF6 to the enrichment process;

b.

Desublimers or cold traps, used to remove UF6 from the enrichment process for subsequent transfer upon heating;

c.

Product and tails stations for transferring UF6 into containers;

d.

Liquefaction or solidification stations used to remove UF6 from the enrichment process by compressing, cooling and converting UF6 to a liquid or solid form;

e.

Piping systems and header systems specially designed or prepared for handling UF6 within gaseous diffusion, centrifuge or aerodynamic cascades;

f.

Vacuum systems and pumps as follows:

1.

Vacuum manifolds, vacuum headers or vacuum pumps having a suction capacity of 5 m3/minute or more;

2.

Vacuum pumps specially designed for use in UF6 bearing atmospheres made of, or protected by, "materials resistant to corrosion by UF6"; or

3.

Vacuum systems consisting of vacuum manifolds, vacuum headers and vacuum pumps, and designed for service in UF6-bearing atmospheres;

g.

UF6 mass spectrometers/ion sources capable of taking on-line samples from UF6 gas streams and having all of the following:

1.

Capable of measuring ions of 320 atomic mass units or greater and having a resolution of better than 1 part in 320;

2.

Ion sources constructed of or protected by nickel, nickel-copper alloys with a nickel content of 60 % or more by weight, or nickel-chrome alloys;

3.

Electron bombardment ionisation sources; and

4.

Having a collector system suitable for isotopic analysis.

[0B003] Plant for the conversion of uranium and equipment specially designed or prepared therefor, as follows:

a.

Systems for the conversion of uranium ore concentrates to UO3;

b.

Systems for the conversion of UO3 to UF6;

c.

Systems for the conversion of UO3 to UO2;

d.

Systems for the conversion of UO2 to UF4;

e.

Systems for the conversion of UF4 to UF6;

f.

Systems for the conversion of UF4 to uranium metal;

g.

Systems for the conversion of UF6 to UO2;

h.

Systems for the conversion of UF6 to UF4;

i.

Systems for the conversion of UO2 to UCl4.

[0B004] Plant for the production or concentration of heavy water, deuterium and deuterium compounds and specially designed or prepared equipment and components therefor, as follows:

a.

Plant for the production of heavy water, deuterium or deuterium compounds, as follows:

1.

Water-hydrogen sulphide exchange plants;

2.

Ammonia-hydrogen exchange plants;

b.

Equipment and components, as follows:

1.

Water-hydrogen sulphide exchange towers with diameters of 1,5 m or more, capable of operating at pressures greater than or equal to 2 MPa;

2.

Single stage, low head (i.e. 0,2 MPa) centrifugal blowers or compressors for hydrogen sulphide gas circulation (i.e. gas containing more than 70 % H2S) with a throughput capacity greater than or equal to 56 m3/second when operating at pressures greater than or equal to 1,8 MPa suction and having seals designed for wet H2S service;

3.

Ammonia-hydrogen exchange towers greater than or equal to 35 m in height with diameters of 1,5 m to 2,5 m capable of operating at pressures greater than 15 MPa;

4.

Tower internals, including stage contactors, and stage pumps, including those which are submersible, for heavy water production utilizing the ammonia-hydrogen exchange process;

5.

Ammonia crackers with operating pressures greater than or equal to 3 MPa for heavy water production utilizing the ammonia-hydrogen exchange process;

6.

Infrared absorption analysers capable of on-line hydrogen/deuterium ratio analysis where deuterium concentrations are equal to or greater than 90 %;

7.

Catalytic burners for the conversion of enriched deuterium gas into heavy water utilizing the ammonia-hydrogen exchange process;

8.

Complete heavy water upgrade systems, or columns therefor, for the upgrade of heavy water to reactor-grade deuterium concentration;

9.

Ammonia synthesis converters or synthesis units specially designed or prepared for heavy water production utilizing the ammonia-hydrogen exchange process.

[0B005] Plant specially designed for the fabrication of "nuclear reactor" fuel elements and specially designed or prepared equipment therefor.

Technical Note:

Specially designed or prepared equipment for the fabrication of "nuclear reactor" fuel elements includes equipment which:

1.

Normally comes into direct contact with or directly processes or controls the production flow of nuclear materials;

2.

Seals the nuclear materials within the cladding;

3.

Checks the integrity of the cladding or the seal;

4.

Checks the finish treatment of the sealed fuel; or

5.

Is used for assembling reactor elements.

[0B006] Plant for the reprocessing of irradiated "nuclear reactor" fuel elements, and specially designed or prepared equipment and components therefor.

Note: 0B006 includes:
a.

Plant for the reprocessing of irradiated "nuclear reactor" fuel elements including equipment and components which normally come into direct contact with and directly control the irradiated fuel and the major nuclear material and fission product processing streams;

b.

Fuel element chopping or shredding machines, i.e. remotely operated equipment to cut, chop or shear irradiated "nuclear reactor" fuel assemblies, bundles or rods;

c.

Dissolvers, critically safe tanks (e.g. small diameter, annular or slab tanks) specially designed or prepared for the dissolution of irradiated "nuclear reactor" fuel, which are capable of withstanding hot, highly corrosive liquids, and which can be remotely loaded and maintained;

d.

Solvent extractors, such as packed or pulsed columns, mixer settlers or centrifugal contractors, resistant to the corrosive effects of nitric acid and specially designed or prepared for use in a plant for the reprocessing of irradiated "natural uranium", "depleted uranium" or "special fissile materials";

[0B007] Plant for the conversion of plutonium and equipment specially designed or prepared therefor, as follows:

a.

Systems for the conversion of plutonium nitrate to oxide;

b.

Systems for plutonium metal production.

[0C] Materials

[0C001] "Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;

Note: 0C001 does not control the following:
a.

Four grammes or less of "natural uranium" or "depleted uranium" when contained in a sensing component in instruments;

b.

"Depleted uranium" specially fabricated for the following civil non-nuclear applications:

1.

Shielding;

2.

Packaging;

3.

Ballasts having a mass not greater than 100 kg;

4.

Counter-weights having a mass not greater than 100 kg;

c.

Alloys containing less than 5 % thorium;

d.

Ceramic products containing thorium, which have been manufactured for non-nuclear use.

[0C002] "Special fissile materials"

Note: 0C002 does not control four "effective grammes" or less when contained in a sensing component in instruments.

[0C003] Deuterium, heavy water (deuterium oxide) and other compounds of deuterium, and mixtures and solutions containing deuterium, in which the isotopic ratio of deuterium to hydrogen exceeds 1:5 000.

[0C004] Graphite having a purity level better than 5 parts per million 'boron equivalent' and with a density greater than 1,50 g/cm3 for use in a "nuclear reactor", in quantities exceeding 1 kg.

N.B.: SEE ALSO 1C107
Note 1: For the purpose of export control, the competent authorities of the Member State in which the exporter is established will determine whether or not the exports of graphite meeting the above specifications are for "nuclear reactor" use.
Note 2: In 0C004, 'boron equivalent' (BE) is defined as the sum of BEz for impurities (excluding BEcarbon since carbon is not considered an impurity) including boron, where:

BEZ (ppm) = CF × concentration of element Z in ppm;

and σB and σZ are the thermal neutron capture cross sections (in barns) for naturally occurring boron and element Z respectively; and AB and AZ are the atomic masses of naturally occurring boron and element Z respectively.

[0C005] Specially prepared compounds or powders for the manufacture of gaseous diffusion barriers, resistant to corrosion by UF6 (e.g. nickel or alloy containing 60 weight per cent or more nickel, aluminium oxide and fully fluorinated hydrocarbon polymers), having a purity of 99,9 % by weight or more and a particle size less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard and a high degree of particle size uniformity.

[0D] Software

[0D001] "Software" specially designed or modified for the "development", "production" or "use" of goods specified in this Category.

[0E] Technology

[0E001] "Technology" according to the Nuclear Technology Note for the "development", "production" or "use" of goods specified in this Category.

CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT
[1A] Systems, Equipment and Components

[1A001] Components made from fluorinated compounds, as follows:

[1A002] "Composite" structures or laminates, having any of the following:

N.B: SEE ALSO 1A202, 9A010 and 9A110
a.

Consisting of an organic "matrix" and materials specified in 1C010.c., 1C010.d. or 1C010.e.; or

b.

Consisting of a metal or carbon "matrix", and any of the following:

1.

Carbon "fibrous or filamentary materials" having all of the following:

a.

A "specific modulus" exceeding 10,15 × 106 m; and

b.

A "specific tensile strength" exceeding 17,7 × 104 m; or

2.

Materials specified in 1C010.c.

Note 1: 1A002 does not control composite structures or laminates made from epoxy resin impregnated carbon "fibrous or filamentary materials" for the repair of "civil aircraft" structures or laminates, having all of the following:
a.

An area not exceeding 1 m2;

b.

A length not exceeding 2,5 m; and

c.

A width exceeding 15 mm.

[1A003] Manufactures of non-"fusible" aromatic polyimides in film, sheet, tape or ribbon form having any of the following:

a.

A thickness exceeding 0,254 mm; or

b.

Coated or laminated with carbon, graphite, metals or magnetic substances.

Note: 1A003 does not control manufactures when coated or laminated with copper and designed for the production of electronic printed circuit boards.
N.B.: For "fusible" aromatic polyimides in any form, see 1C008.a.3.

[1A004] Protective and detection equipment and components not specially designed for military use, as follows:

N.B.: SEE ALSO MILITARY GOODS CONTROLS, 2B351 AND 2B352.
a.

Full face masks, filter canisters and decontamination equipment therefor, designed or modified for defence against any of the following, and specially designed components therefor:

Note: 1A004.a. includes Powered Air Purifying Respirators (PAPR) that are designed or modified for defence against agents or materials, listed in 1A004.a.
Technical Note:

'Trace detection' is defined as the capability to detect less than 1 ppm vapour, or 1 mg solid or liquid.

Note 1: 1A004.d. does not control equipment specially designed for laboratory use.
Note 2: 1A004.d. does not control non-contact walk-through security portals.
Note: 1A004 does not control:
a.

Personal radiation monitoring dosimeters;

b.

Occupational health or safety equipment limited by design or function to protect against hazards specific to residential safety or civil industries, including:

1.

mining;

2.

quarrying;

3.

agriculture;

4.

pharmaceutical;

5.

medical;

6.

veterinary;

7.

environmental;

8.

waste management;

9.

food industry.

Technical Notes:
1.

1A004 includes equipment and components that have been identified, successfully tested to national standards or otherwise proven effective, for the detection of or defence against radioactive materials "adapted for use in war", biological agents "adapted for use in war", chemical warfare agents, 'simulants' or "riot control agents", even if such equipment or components are used in civil industries such as mining, quarrying, agriculture, pharmaceuticals, medical, veterinary, environmental, waste management, or the food industry.

2.

'Simulant' is a substance or material that is used in place of toxic agent (chemical or biological) in training, research, testing or evaluation.

[1A005] Body armour and components therefor, as follows:

N.B.: SEE ALSO MILITARY GOODS CONTROLS.
a.

Soft body armour not manufactured to military standards or specifications, or to their equivalents, and specially designed components therefor;

b.

Hard body armour plates providing ballistic protection equal to or less than level IIIA (NIJ 0101.06, July 2008) or national equivalents.

N.B.: For "fibrous or filamentary materials" used in the manufacture of body armour, see 1C010.
Note 1: 1A005 does not control body armour when accompanying its user for the user's own personal protection.
Note 2: 1A005 does not control body armour designed to provide frontal protection only from both fragment and blast from non-military explosive devices.
Note 3: 1A005 does not control body armour designed to provide protection only from knife, spike, needle or blunt trauma.

[1A006] Equipment, specially designed or modified for the disposal of improvised explosive devices, as follows, and specially designed components and accessories therefor:

N.B.: SEE ALSO MILITARY GOODS CONTROLS.
a.

Remotely operated vehicles;

b.

'Disruptors'.

Technical Note:

'Disruptors' are devices specially designed for the purpose of preventing the operation of an explosive device by projecting a liquid, solid or frangible projectile.

Note: 1A006 does not control equipment when accompanying its operator.

[1A007] Equipment and devices, specially designed to initiate charges and devices containing "energetic materials", by electrical means, as follows:

N.B.: SEE ALSO MILITARY GOODS CONTROLS, 3A229 AND 3A232.
a.

Explosive detonator firing sets designed to drive explosive detonators specified in 1A007.b.;

b.

Electrically driven explosive detonators as follows:

1.

Exploding bridge (EB);

2.

Exploding bridge wire (EBW);

3.

Slapper;

4.

Exploding foil initiators (EFI).

Technical Notes:
1. The word initiator or igniter is sometimes used in place of the word detonator.
2. For the purpose of 1A007.b. the detonators of concern all utilise a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporises when a fast, high-current electrical pulse is passed through it. In non-slapper types, the exploding conductor starts a chemical detonation in a contacting high explosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator.

[1A008] Charges, devices and components, as follows:

a.

'Shaped charges' having all of the following:

1.

Net Explosive Quantity (NEQ) greater than 90 g; and

2.

Outer casing diameter equal to or greater than 75 mm;

b.

Linear shaped cutting charges having all of the following, and specially designed components therefor:

1.

An explosive load greater than 40 g/m; and

2.

A width of 10 mm or more;

c.

Detonating cord with explosive core load greater than 64 g/m;

d.

Cutters, other than those specified in 1A008.b., and severing tools, having a Net Explosive Quantity (NEQ) greater than 3,5 kg.

Technical Note:

'Shaped charges' are explosive charges shaped to focus the effects of the explosive blast.

[1A102] Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

[1A202] Composite structures, other than those specified in 1A002, in the form of tubes and having both of the following characteristics:

N.B.: SEE ALSO 9A010 AND 9A110.
a.

An inside diameter of between 75 mm and 400 mm; and

b.

Made with any of the "fibrous or filamentary materials" specified in 1C010.a. or b. or 1C210.a. or with carbon prepreg materials specified in 1C210.c.

[1A225] Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.

[1A226] Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:

a.

Made of phosphor bronze mesh chemically treated to improve wettability; and

b.

Designed to be used in vacuum distillation towers.

[1A227] High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:

a.

A 'cold area' greater than 0,09 m2;

b.

A density greater than 3 g/cm3; and

c.

A thickness of 100 mm or greater.

Technical Note:

In 1A227 the term 'cold area' means the viewing area of the window exposed to the lowest level of radiation in the design application.

[1B] Test, Inspection and Production Equipment

[1B001] Equipment for the production or inspection of "composite" structures or laminates specified in 1A002 or "fibrous or filamentary materials" specified in 1C010, as follows, and specially designed components and accessories therefor:

N.B.: SEE ALSO 1B101 AND 1B201.
a.

Filament winding machines, of which the motions for positioning, wrapping and winding fibres are coordinated and programmed in three or more 'primary servo positioning' axes, specially designed for the manufacture of "composite" structures or laminates, from "fibrous or filamentary materials";

b.

'Tape-laying machines', of which the motions for positioning and laying tape are coordinated and programmed in five or more 'primary servo positioning' axes, specially designed for the manufacture of "composite" airframe or 'missile' structures;

Note: In 1B001.b. 'missile' means complete rocket systems and unmanned aerial vehicle systems.

Multidirectional, multidimensional weaving machines or interlacing machines, including adapters and modification kits, specially designed or modified for weaving, interlacing or braiding fibres, for "composite" structures;

Technical Note:

For the purposes of 1B001.g., 'tow-placement machines' have the ability to place one or more 'filament bands' having widths less than or equal to 25 mm, and to cut and restart individual 'filament band' courses during the placement process.

Technical Note:
1. For the purpose of 1B001, 'primary servo positioning' axes control, under computer program direction, the position of the end effector (i.e., head) in space relative to the work piece at the correct orientation and direction to achieve the desired process.
2. For the purposes of 1B001., a 'filament band' is a single continuous width of fully or partially resin-impregnated tape, tow or fibre.

[1B002] Equipment for producing metal alloys, metal alloy powder or alloyed materials, specially designed to avoid contamination and specially designed for use in one of the processes specified in 1C002.c.2.

N.B.: SEE ALSO 1B102.

[1B003] Tools, dies, moulds or fixtures, for "superplastic forming" or "diffusion bonding" titanium, aluminium or their alloys, specially designed for the manufacture of any of the following:

a.

Airframe or aerospace structures;

b.

"Aircraft" or aerospace engines; or

c.

Specially designed components for structures specified in 1B003.a. or for engines specified in 1B003.b.

[1B101] Equipment, other than that specified in 1B001, for the "production" of structural composites as follows; and specially designed components and accessories therefor:

N.B.: SEE ALSO 1B201.
Note: Components and accessories specified in 1B101 include moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof.

[1B102] Metal powder "production equipment", other than that specified in 1B002, and components as follows:

N.B.: SEE ALSO 1B115.b.
a.

Metal powder "production equipment" usable for the "production", in a controlled environment, of spherical, spheroidal or atomised materials specified in 1C011.a., 1C011.b., 1C111.a.1., 1C111.a.2. or in the Military Goods Controls.

b.

Specially designed components for "production equipment" specified in 1B002 or 1B102.a.

Note: 1B102 includes:
a.

Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;

b.

Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;

c.

Equipment usable for the "production" of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen).

[1B115] Equipment, other than that specified in 1B002 or 1B102, for the production of propellant and propellant constituents, as follows, and specially designed components therefor:

Note 1: For equipment specially designed for the production of military goods, see the Military Goods Controls.
Note 2: 1B115 does not control equipment for the "production", handling and acceptance testing of boron carbide.

[1B116] Specially designed nozzles for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1 573 K (1 300 °C) to 3 173 K (2 900 °C) temperature range at pressures of 130 Pa to 20 kPa.

[1B117] Batch mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with temperature control capability of the mixing chamber and having all of the following, and specially designed components therefor:

a.

A total volumetric capacity of 110 litres or more; and

b.

At least one 'mixing/kneading shaft' mounted off centre.

Note: In 1B117.b. the term 'mixing/kneading shaft' does not refer to deagglomerators or knife-spindles.

[1B118] Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following, and specially designed components therefor:

a.

Two or more mixing/kneading shafts; or

b.

A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber.

[1B119] Fluid energy mills usable for grinding or milling substances specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls, and specially designed components therefor.

[1B201] Filament winding machines, other than those specified in 1B001 or 1B101, and related equipment, as follows:

a.

Filament winding machines having all of the following characteristics:

1.

Having motions for positioning, wrapping, and winding fibres coordinated and programmed in two or more axes;

2.

Specially designed to fabricate composite structures or laminates from "fibrous or filamentary materials"; and

3.

Capable of winding cylindrical tubes with an internal diameter between 75 and 650 mm and lengths of 300 mm or greater;

b.

Coordinating and programming controls for the filament winding machines specified in 1B201.a.;

c.

Precision mandrels for the filament winding machines specified in 1B201.a.

[1B225] Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.

[1B226] Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.

Note: 1B226 includes separators:
a.

Capable of enriching stable isotopes;

b.

With the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.

[1B228] Hydrogen-cryogenic distillation columns having all of the following characteristics:

a.

Designed for operation with internal temperatures of 35 K (– 238 °C) or less;

b.

Designed for operation at an internal pressure of 0,5 to 5 MPa;

c.

Constructed of either:

1.

Stainless steel of the 300 series with low sulphur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or

2.

Equivalent materials which are both cryogenic and H2-compatible; and

d.

With internal diameters of 30 cm or greater and 'effective lengths' of 4 m or greater.

Technical Note:

In 1B228 'effective length' means the active height of packing material in a packed-type column, or the active height of internal contactor plates in a plate-type column.

[1B229] Water-hydrogen sulphide exchange tray columns and 'internal contactors', as follows:

N.B.: For columns which are specially designed or prepared for the production of heavy water see 0B004.

[1B230] Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:

a.

Airtight (i.e., hermetically sealed);

b.

A capacity greater than 8,5 m3/h; and

c.

Either of the following characteristics:

1.

For concentrated potassium amide solutions (1 % or greater), an operating pressure of 1,5 to 60 MPa; or

2.

For dilute potassium amide solutions (less than 1 %), an operating pressure of 20 to 60 MPa.

[1B231] Tritium facilities or plants, and equipment therefor, as follows:

a.

Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;

b.

Equipment for tritium facilities or plants, as follows:

1.

Hydrogen or helium refrigeration units capable of cooling to 23 K (– 250 °C) or less, with heat removal capacity greater than 150 W;

2.

Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.

[1B232] Turboexpanders or turboexpander-compressor sets having both of the following characteristics:

a.

Designed for operation with an outlet temperature of 35 K (– 238 °C) or less; and

b.

Designed for a throughput of hydrogen gas of 1 000 kg/h or greater.

[1B233] Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows:

a.

Facilities or plants for the separation of lithium isotopes;

b.

Equipment for the separation of lithium isotopes based on the lithium-mercury amalgam process, as follows:

1.

Packed liquid-liquid exchange columns specially designed for lithium amalgams;

2.

Mercury or lithium amalgam pumps;

3.

Lithium amalgam electrolysis cells;

4.

Evaporators for concentrated lithium hydroxide solution;

c.

Ion exchange systems specially designed for lithium isotope separation, and specially designed components therefor;

d.

Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers), specially designed for lithium isotope separation, and specially designed components therefor.

[1B234] High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics:

N.B.: SEE ALSO MILITARY GOODS CONTROLS.
a.

Designed to fully contain an explosion equivalent to 2 kg of TNT or greater; and

b.

Having design elements or features enabling real time or delayed transfer of diagnostic or measurement information.

[1C] Materials
Technical Note:

Metals and alloys:

Unless provision to the contrary is made, the words 'metals' and 'alloys' in 1C001 to 1C012 cover crude and semi-fabricated forms, as follows:

Crude forms:

Anodes, balls, bars (including notched bars and wire bars), billets, blocks, blooms, brickets, cakes, cathodes, crystals, cubes, dice, grains, granules, ingots, lumps, pellets, pigs, powder, rondelles, shot, slabs, slugs, sponge, sticks;

Semi-fabricated forms (whether or not coated, plated, drilled or punched):

a.

Wrought or worked materials fabricated by rolling, drawing, extruding, forging, impact extruding, pressing, graining, atomising, and grinding, i.e.: angles, channels, circles, discs, dust, flakes, foils and leaf, forging, plate, powder, pressings and stampings, ribbons, rings, rods (including bare welding rods, wire rods, and rolled wire), sections, shapes, sheets, strip, pipe and tubes (including tube rounds, squares, and hollows), drawn or extruded wire;

b.

Cast material produced by casting in sand, die, metal, plaster or other types of moulds, including high pressure castings, sintered forms, and forms made by powder metallurgy.

The object of the control should not be defeated by the export of non-listed forms alleged to be finished products but representing in reality crude forms or semi-fabricated forms.

[1C001] Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as follows:

N.B. SEE ALSO 1C101.
a.

Materials for absorbing frequencies exceeding 2 × 108 Hz but less than 3 × 1012 Hz;

Note 1: 1C001.a. does not control:

Materials for absorbing frequencies exceeding 1,5 × 1014 Hz but less than 3.7 × 1014 Hz and not transparent to visible light;

[1C002] Metal alloys, metal alloy powder and alloyed materials, as follows:

N.B.: SEE ALSO 1C202.
Note: 1C002 does not control metal alloys, metal alloy powder and alloyed materials for coating substrates.
Technical Notes:
1. The metal alloys in 1C002 are those containing a higher percentage by weight of the stated metal than of any other element.
2. 'Stress-rupture life' should be measured in accordance with ASTM standard E-139 or national equivalents.
3. 'Low cycle fatigue life' should be measured in accordance with ASTM Standard E-606 'Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing' or national equivalents. Testing should be axial with an average stress ratio equal to 1 and a stress-concentration factor (Kt) equal to 1. The average stress is defined as maximum stress minus minimum stress divided by maximum stress.
a.

Aluminides, as follows:

1.

Nickel aluminides containing a minimum of 15 % by weight aluminium, a maximum of 38 % by weight aluminium and at least one additional alloying element;

2.

Titanium aluminides containing 10 % by weight or more aluminium and at least one additional alloying element;

b.

Metal alloys, as follows, made from the powder or particulate material specified in 1C002.c.:

1.

Nickel alloys having any of the following:

a.

A 'stress-rupture life' of 10 000 hours or longer at 923 K (650 °C) at a stress of 676 MPa; or

b.

A 'low cycle fatigue life' of 10 000 cycles or more at 823 K (550 °C) at a maximum stress of 1 095 MPa;

2.

Niobium alloys having any of the following:

a.

A 'stress-rupture life' of 10 000 hours or longer at 1 073 K (800 °C) at a stress of 400 MPa; or

b.

A 'low cycle fatigue life' of 10 000 cycles or more at 973 K (700 °C) at a maximum stress of 700 MPa;

3.

Titanium alloys having any of the following:

a.

A 'stress-rupture life' of 10 000 hours or longer at 723 K (450 °C) at a stress of 200 MPa; or

b.

A 'low cycle fatigue life' of 10 000 cycles or more at 723 K (450 °C) at a maximum stress of 400 MPa;

4.

Aluminium alloys having any of the following:

a.

A tensile strength of 240 MPa or more at 473 K (200 °C); or

b.

A tensile strength of 415 MPa or more at 298 K (25 °C);

5.

Magnesium alloys having all of the following:

a.

A tensile strength of 345 MPa or more; and

b.

A corrosion rate of less than 1 mm/year in 3 % sodium chloride aqueous solution measured in accordance with ASTM standard G-31 or national equivalents;

[1C003] Magnetic metals, of all types and of whatever form, having any of the following:

[1C004] Uranium titanium alloys or tungsten alloys with a "matrix" based on iron, nickel or copper, having all of the following:

a.

A density exceeding 17,5 g/cm3;

b.

An elastic limit exceeding 880 MPa;

c.

An ultimate tensile strength exceeding 1 270 MPa; and

d.

An elongation exceeding 8 %.

[1C005] "Superconductive" "composite" conductors in lengths exceeding 100 m or with a mass exceeding 100 g, as follows:

[1C006] Fluids and lubricating materials, as follows:

a.

Hydraulic fluids containing, as their principal ingredients, any of the following:

Technical Note:

For the purpose of 1C006:

1.

'Flash point' is determined using the Cleveland Open Cup Method described in ASTM D-92 or national equivalents;

2.

'Pour point' is determined using the method described in ASTM D-97 or national equivalents;

3.

'Viscosity index' is determined using the method described in ASTM D-2270 or national equivalents;

4.

'Thermal stability' is determined by the following test procedure or national equivalents:

Twenty ml of the fluid under test is placed in a 46 ml type 317 stainless steel chamber containing one each of 12,5 mm (nominal) diameter balls of M-10 tool steel, 52100 steel and naval bronze (60 % Cu, 39 % Zn, 0,75 % Sn);

The chamber is purged with nitrogen, sealed at atmospheric pressure and the temperature raised to and maintained at 644 ± 6 K (371 ± 6 °C) for six hours;

The specimen will be considered thermally stable if, on completion of the above procedure, all of the following conditions are met:

a.

The loss in weight of each ball is less than 10 mg/mm2 of ball surface;

b.

The change in original viscosity as determined at 311 K (38 °C) is less than 25 %; and

c.

The total acid or base number is less than 0,40;

5.

'Autogenous ignition' temperature is determined using the method described in ASTM E-659 or national equivalents.

[1C007] [X1Ceramic powders, non-"composite" ceramic materials, ceramic-"matrix" "composite" materials and precursor materials, as follows:]

N.B.: SEE ALSO 1C107.
a.

Ceramic powders of single or complex borides of titanium, having total metallic impurities, excluding intentional additions, of less than 5 000 ppm, an average particle size equal to or less than 5 μm and no more than 10 % of the particles larger than 10 μm;

b.

Non-"composite" ceramic materials in crude or semi-fabricated form, composed of borides of titanium with a density of 98 % or more of the theoretical density;

[1C008] Non-fluorinated polymeric substances as follows:

Technical Note:
1.

The 'glass transition temperature (Tg)' for 1C008.a.2. thermoplastic materials and 1C008.a.4. materials is determined using the method described in ISO 11357-2 (1999) or national equivalents

2.

The 'glass transition temperature (Tg)' for 1C008.a.2. thermosetting materials and 1C008.a.3. materials is determined using the 3-point bend method described in ASTM D 7028-07 or equivalent national standard. The test is to be performed using a dry test specimen which has attained a minimum of 90 % degree of cure as specified by ASTM E 2160-04 or equivalent national standard, and was cured using the combination of standard- and post-cure processes that yield the highest Tg.

[1C009] Unprocessed fluorinated compounds as follows:

a.

Copolymers of vinylidene fluoride having 75 % or more beta crystalline structure without stretching;

b.

Fluorinated polyimides containing 10 % by weight or more of combined fluorine;

c.

Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine.

[1C010] "Fibrous or filamentary materials", as follows:

N.B.: SEE ALSO 1C210 AND 9C110.
Technical Notes:
1.

For the purpose of calculating "specific tensile strength", "specific modulus" or specific weight of "fibrous or filamentary materials" in 1C010.a., 1C010.b., 1C010.c. or 1C010.e.1.b., the tensile strength and modulus should be determined by using Method A described in ISO 10618 (2004) or national equivalents.

2.

Assessing the "specific tensile strength", "specific modulus" or specific weight of non-unidirectional "fibrous or filamentary materials" (e.g., fabrics, random mats or braids) in 1C010 is to be based on the mechanical properties of the constituent unidirectional monofilaments (e.g., monofilaments, yarns, rovings or tows) prior to processing into the non-unidirectional "fibrous or filamentary materials".

a.

Organic "fibrous or filamentary materials", having all of the following:

1.

"Specific modulus" exceeding 12,7 × 106 m; and

2.

"Specific tensile strength" exceeding 23,5 × 104 m;

Carbon "fibrous or filamentary materials", having all of the following:

Inorganic "fibrous or filamentary materials", having all of the following:

Fully or partially resin-impregnated or pitch-impregnated "fibrous or filamentary materials" (prepregs), metal or carbon-coated "fibrous or filamentary materials" (preforms) or "carbon fibre preforms", having all of the following:

Having any of the following:

[1C011] Metals and compounds, as follows:

N.B.: SEE ALSO MILITARY GOODS CONTROLS and 1C111.
a.

Metals in particle sizes of less than 60 μm whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of zirconium, magnesium and alloys thereof;

Technical Note:

The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.

[1C012] Materials as follows:

Technical Note:

These materials are typically used for nuclear heat sources.

[1C101] Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified in 1C001, usable in 'missiles', "missile" subsystems or unmanned aerial vehicles specified in 9A012 or 9A112.a.

Note 1: 1C101 includes:
a.

Structural materials and coatings specially designed for reduced radar reflectivity;

b.

Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet regions of the electromagnetic spectrum.

Note 2: 1C101 does not include coatings when specially used for the thermal control of satellites.
Technical Note:

In 1C101 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[1C102] Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

[1C107] Graphite and ceramic materials, other than those specified in 1C007, as follows:

[1C111] Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:

a.

Propulsive substances:

1.

Spherical or spheroidal aluminium powder other than that specified in the Military Goods Controls, in particle size of less than 200 μm and an aluminium content of 97 % by weight or more, if at least 10 % of the total weight is made up of particles of less than 63 μm, according to ISO 2591-1:1988 or national equivalents;

Metal powders, other than that specified in the Military Goods Controls, as follows:

Oxidiser substances usable in liquid propellant rocket engines as follows:

Hydrazine derivatives as follows:

Polymeric substances:

Other propellant additives and agents:

[1C116] Maraging steels, useable in 'missiles', having all of the following:

N.B.: SEE ALSO 1C216.
a.

Having an ultimate tensile strength, measured at 293 K (20 °C), equal to or greater than:

1.

0,9 GPa in the solution annealed stage; or

2.

1,5 GPa in the precipitation hardened stage; and

b.

Any of the following forms:

1.

Sheet, plate or tubing with a wall or plate thickness equal to or less than 5,0 mm;

2.

Tubular forms with a wall thickness equal to or less than 50 mm and having an inner diameter equal to or greater than 270 mm.

Technical Note 1:

Maraging steels are iron alloy:

1.

Generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce strengthening and age-hardening of the alloy; and

2.

Subjected to heat treatment cycles to facilitate the martensitic transformation process (solution annealed stage) and subsequently age hardened (precipitation hardened stage).

Technical Note 2:

In 1C116 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[1C117] Materials for the fabrication of 'missiles' components as follows:

a.

Tungsten and alloys in particulate form with a tungsten content of 97 % by weight or more and a particle size of 50 × 10–6 m (50 μm) or less;

b.

Molybdenum and alloys in particulate form with a molybdenum content of 97 % by weight or more and a particle size of 50 × 10–6 m (50 μm) or less;

c.

Tungsten materials in solid form having all of the following:

1.

Any of the following material compositions:

a.

Tungsten and alloys containing 97 % by weight or more of tungsten;

b.

Copper infiltrated tungsten containing 80 % by weight or more of tungsten; or

c.

Silver infiltrated tungsten containing 80 % by weight ot more of tungsten; and

2.

Able to be machined to any of the following products:

a.

Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;

b.

Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or

c.

Blocks having a size of 120 mm by 120 mm by 50 mm or greater.

Technical Note:

In 1C117 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[1C118] Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:

a.

Having all of the following characteristics:

1.

Containing 17,0 - 23,0 weight percent chromium and 4,5 - 7,0 weight percent nickel;

2.

Having a titanium content of greater than 0,10 weight percent; and

3.

A ferritic-austenitic microstructure (also referred to as a two-phase microstructure) of which at least 10 percent is austenite by volume (according to ASTM E-1181-87 or national equivalents); and

b.

Having any of the following forms:

1.

Ingots or bars having a size of 100 mm or more in each dimension;

2.

Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or

3.

Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less.

[1C202] Alloys, other than those specified in 1C002.b.3. or.b.4., as follows:

a.

Aluminium alloys having both of the following characteristics:

1.

'Capable of' an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); and

2.

In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm;

b.

Titanium alloys having both of the following characteristics:

1.

'Capable of' an ultimate tensile strength of 900 MPa or more at 293 K (20 °C); and

2.

In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.

Technical Note:

The phrase alloys 'capable of' encompasses alloys before or after heat treatment.

[1C210] 'Fibrous or filamentary materials' or prepregs, other than those specified in 1C010.a., b. or e., as follows:

Note: In 1C210, 'fibrous or filamentary materials' is restricted to continuous "monofilaments", "yarns", "rovings", "tows" or "tapes".

[1C216] Maraging steel, other than that specified in 1C116, 'capable of' an ultimate tensile strength of 1 950 MPa or more, at 293 K (20 °C).

Note: 1C216 does not control forms in which all linear dimensions are 75 mm or less.
Technical Note:

The phrase maraging steel 'capable of' encompasses maraging steel before or after heat treatment.

[1C225] Boron enriched in the boron-10 (10B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.

Note: In 1C225 mixtures containing boron include boron loaded materials.
Technical Note:

The natural isotopic abundance of boron-10 is approximately 18,5 weight per cent (20 atom per cent).

[1C226] Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, other than that specified by 1C117, having both of the following characteristics:

a.

In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm; and

b.

A mass greater than 20 kg.

Note: 1C226 does not control manufactures specially designed as weights or gamma-ray collimators.

[1C227] Calcium having both of the following characteristics:

a.

Containing less than 1 000 parts per million by weight of metallic impurities other than magnesium; and

b.

Containing less than 10 parts per million by weight of boron.

[1C228] Magnesium having both of the following characteristics:

a.

Containing less than 200 parts per million by weight of metallic impurities other than calcium; and

b.

Containing less than 10 parts per million by weight of boron.

[1C229] Bismuth having both of the following characteristics:

a.

A purity of 99,99 % or greater by weight; and

b.

Containing less than 10 ppm (parts per million) by weight of silver.

[1C230] Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing, other than that specified in the Military Goods Controls.

N.B.: SEE ALSO MILITARY GOODS CONTROLS.
Note: 1C230 does not control the following:
a.

Metal windows for X-ray machines, or for bore-hole logging devices;

b.

Oxide shapes in fabricated or semi-fabricated forms specially designed for electronic component parts or as substrates for electronic circuits;

c.

Beryl (silicate of beryllium and aluminium) in the form of emeralds or aquamarines.

[1C231] Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.

[1C232] Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.

Note: 1C232 does not control a product or device containing less than 1 g of helium-3.

[1C233] Lithium enriched in the lithium-6 (6Li) isotope to greater than its natural isotopic abundance, and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.

Note: 1C233 does not control thermoluminescent dosimeters.
Technical Note:

The natural isotopic abundance of lithium-6 is approximately 6,5 weight per cent (7.5 atom per cent).

[1C234] Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing, other than those specified in 0A001.f.

Note: 1C234 does not control zirconium in the form of foil having a thickness of 0,10 mm or less.

[1C235] Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1 000, and products or devices containing any of the foregoing.

Note: 1C235 does not control a product or device containing less than 1.48 × 103 GBq (40 Ci) of tritium.

[1C236] 'Radionuclides' appropriate for making neutron sources based on alpha-n reaction, other than those specified in 0C001 and 1C012.a., in the following forms:

a.

Elemental;

b.

Compounds having a total activity of 37 GBq/kg (1 Ci/kg) or greater;

c.

Mixtures having a total activity of 3 GBq/kg (1 Ci/kg) or greater;

d.

Products or devices containing any of the foregoing.

Note: 1C236 does not control a product or device containing less than 3,7 GBq (100 millicuries) of activity.
Technical Note:

In 1C236 'radionuclides' are any of the following:

  • Actinium-225 (Ac-225)

  • Actinium-227 (Ac-227)

  • Californium-253 (Cf-253)

  • Curium-240 (Cm-240)

  • Curium-241 (Cm-241)

  • Curium-242 (Cm-242)

  • Curium-243 (Cm-243)

  • Curium-244 (Cm-244)

  • Einsteinium-253 (Es-253)

  • Einsteinium-254 (Es-254)

  • Gadolinium-148 (Gd-148)

  • Plutonium-236 (Pu-236)

  • Plutonium-238 (Pu-238)

  • Polonium-208 (Po-208)

  • Polonium-209 (Po-209)

  • Polonium-210 (Po-210)

  • Radium-223 (Ra-223)

  • Thorium-227 (Th-227)

  • Thorium-228 (Th-228)

  • Uranium-230 (U-230)

  • Uranium-232 (U-232)

[1C237] Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing.

Note: 1C237 does not control the following:
a.

Medical applicators;

b.

A product or device containing less than 0,37 GBq (10 millicuries) of radium-226.

[1C238] Chlorine trifluoride (ClF3).

[1C239] High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8 000 m/s.

[1C240] Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:

a.

Nickel powder having both of the following characteristics:

1.

A nickel purity content of 99,0 % or greater by weight; and

2.

A mean particle size of less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard;

b.

Porous nickel metal produced from materials specified in 1C240.a.

Note: 1C240 does not control the following:
a.

Filamentary nickel powders;

b.

Single porous nickel sheets with an area of 1 000 cm2 per sheet or less.

Technical Note:

1C240.b. refers to porous metal formed by compacting and sintering the materials in 1C240.a. to form a metal material with fine pores interconnected throughout the structure.

[1C241] Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, other than those specified in 1C226, having both of the following characteristics:

a.

In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; and

b.

A mass greater than 20 kg.

[1C350] Chemicals, which may be used as precursors for toxic chemical agents, as follows, and "chemical mixtures" containing one or more thereof:

N.B.: SEE ALSO MILITARY GOODS CONTROLS AND 1C450.
1.

Thiodiglycol (111-48-8);

2.

Phosphorus oxychloride (10025-87-3);

3.

Dimethyl methylphosphonate (756-79-6);

4.

SEE MILITARY GOODS CONTROLS for Methyl phosphonyl difluoride (676-99-3);

5.

Methyl phosphonyl dichloride (676-97-1);

6.

Dimethyl phosphite (DMP) (868-85-9);

7.

Phosphorus trichloride (7719-12-2);

8.

Trimethyl phosphite (TMP) (121-45-9);

9.

Thionyl chloride (7719-09-7);

10.

3-Hydroxy-1-methylpiperidine (3554-74-3);

11.

N,N-Diisopropyl-(beta)-aminoethyl chloride (96-79-7);

12.

N,N-Diisopropyl-(beta)-aminoethane thiol (5842-07-9);

13.

3-Quinuclidinol (1619-34-7);

14.

Potassium fluoride (7789-23-3);

15.

2-Chloroethanol (107-07-3);

16.

Dimethylamine (124-40-3);

17.

Diethyl ethylphosphonate (78-38-6);

18.

Diethyl N,N-dimethylphosphoramidate (2404-03-7);

19.

Diethyl phosphite (762-04-9);

20.

Dimethylamine hydrochloride (506-59-2);

21.

Ethyl phosphinyl dichloride (1498-40-4);

22.

Ethyl phosphonyl dichloride (1066-50-8);

23.

SEE MILITARY GOODS CONTROLS for Ethyl phosphonyl difluoride (753-98-0);

24.

Hydrogen fluoride (7664-39-3);

25.

Methyl benzilate (76-89-1);

26.

Methyl phosphinyl dichloride (676-83-5);

27.

N,N-Diisopropyl-(beta)-amino ethanol (96-80-0);

28.

Pinacolyl alcohol (464-07-3);

29.

SEE MILITARY GOODS CONTROLS for O-Ethyl-O-2-diisopropylaminoethyl methyl phosphonite (QL) (57856-11-8);

30.

Triethyl phosphite (122-52-1);

31.

Arsenic trichloride (7784-34-1);

32.

Benzilic acid (76-93-7);

33.

Diethyl methylphosphonite (15715-41-0);

34.

Dimethyl ethylphosphonate (6163-75-3);

35.

Ethyl phosphinyl difluoride (430-78-4);

36.

Methyl phosphinyl difluoride (753-59-3);

37.

3-Quinuclidone (3731-38-2);

38.

Phosphorus pentachloride (10026-13-8);

39.

Pinacolone (75-97-8);

40.

Potassium cyanide (151-50-8);

41.

Potassium bifluoride (7789-29-9);

42.

Ammonium hydrogen fluoride or ammonium bifluoride (1341-49-7);

43.

Sodium fluoride (7681-49-4);

44.

Sodium bifluoride (1333-83-1);

45.

Sodium cyanide (143-33-9);

46.

Triethanolamine (102-71-6);

47.

Phosphorus pentasulphide (1314-80-3);

48.

Di-isopropylamine (108-18-9);

49.

Diethylaminoethanol (100-37-8);

50.

Sodium sulphide (1313-82-2);

51.

Sulphur monochloride (10025-67-9);

52.

Sulphur dichloride (10545-99-0);

53.

Triethanolamine hydrochloride (637-39-8);

54.

N,N-Diisopropyl-(Beta)-aminoethyl chloride hydrochloride (4261-68-1);

55.

Methylphosphonic acid (993-13-5);

56.

Diethyl methylphosphonate (683-08-9);

57.

N,N-Dimethylaminophosphoryl dichloride (677-43-0);

58.

Triisopropyl phosphite (116-17-6);

59.

Ethyldiethanolamine (139-87-7);

60.

O,O-Diethyl phosphorothioate (2465-65-8);

61.

O,O-Diethyl phosphorodithioate (298-06-6);

62.

Sodium hexafluorosilicate (16893-85-9);

63.

Methylphosphonothioic dichloride (676-98-2).

Note 1: For exports to "States not Party to the Chemical Weapons Convention", 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57 and .63 in which no individually specified chemical constitutes more than 10 % by the weight of the mixture.
Note 2: For exports to "States Party to the Chemical Weapons Convention", 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57 and .63 in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.
Note 3: 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.2, .6, .7, .8, .9, .10, .14, .15, .16, .19, .20, .24, .25, .30, .37, .38, .39, .40, .41, .42, .43, .44, .45, .46, .47, .48, .49, .50, .51, .52, .53, .58, .59, .60, .61 and .62 in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.
Note 4: 1C350 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.

[1C351] Human and animal pathogens and "toxins", as follows:

a.

Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

1.

African horse sickness virus;

2.

African swine fever virus;

3.

Andes virus;

Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

Note: 1C351 does not control "vaccines" or "immunotoxins".

[1C352] Not used

[1C353] Genetic elements and genetically modified organisms, as follows:

a.

Genetically modified organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity of organisms specified in 1C351.a., 1C351.c, 1C351.e. or 1C354;

b.

Genetically modified organisms or genetic elements that contain nucleic acid sequences coding for any of the "toxins" specified in 1C351.d. or "sub-units of toxins" thereof.

Technical Notes:
1.

Genetically-modified organisms includes organisms in which the genetic material (nucleic acid sequences) has been altered in a way that does not occur naturally by mating and/or natural recombination, and encompasses those produced artificially in whole or in part.

2.

Genetic elements include inter alia chromosomes, genomes, plasmids, transposons, and vectors whether genetically modified or unmodified, or chemically synthesized in whole or in part.

3.

Nucleic acid sequences associated with the pathogenicity of any of the micro-organisms specified in 1C351.a., 1C351.c., 1C351.e. or 1C354 means any sequence specific to the specified micro-organism that:

a.

In itself or through its transcribed or translated products represents a significant hazard to human, animal or plant health; or

b.

Is known to enhance the ability of a specified micro-organism, or any other organism into which it may be inserted or otherwise integrated, to cause serious harm to humans, animals or plant health.

Note: 1C353 does not control nucleic acid sequences associated with the pathogenicity of enterohaemorrhagic Escherichia coli, serotype O157 and other verotoxin producing strains, other than those coding for the verotoxin, or for its sub-units.

[1C354] Plant pathogens, as follows:

a.

Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

1.

Andean potato latent virus (Potato Andean latent tymovirus);

2.

Potato spindle tuber viroid;

b.

Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

1.

Xanthomonas albilineans;

2.

Xanthomonas axonopodis pv. citri (Xanthomonas campestris pv. citri A) [Xanthomonas campestris pv. citri];

3.

Xanthomonas oryzae pv. oryzae (Pseudomonas campestris pv. oryzae);

4.

Clavibacter michiganensis subsp. sepedonicus (Corynebacterium michiganensis subsp. sepedonicum or Corynebacterium sepedonicum);

5.

Ralstonia solanacearum, race 3, biovar 2;

c.

Fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

1.

Colletotrichum kahawae (Colletotrichum coffeanum var. virulans);

2.

Cochliobolus miyabeanus (Helminthosporium oryzae);

3.

Microcyclus ulei (syn. Dothidella ulei);

4.

Puccinia graminis ssp. graminis var. graminis / Puccinia graminis ssp. graminis var. stakmanii (Puccinia graminis [syn. Puccinia graminis f. sp. tritici]);

5.

Puccinia striiformis (syn. Puccinia glumarum);

6.

Magnaporthe oryzae (Pyricularia oryzae);

7.

Peronosclerospora philippinensis (Peronosclerospora sacchari);

8.

Sclerophthora rayssiae var. zeae;

9.

Synchytrium endobioticium;

10.

Tilletia indica;

11.

Thecaphora solani.

[1C450] Toxic chemicals and toxic chemical precursors, as follows, and "chemical mixtures" containing one or more thereof:

N.B.: SEE ALSO ENTRY 1C350, 1C351.d. AND MILITARY GOODS CONTROLS.
a.

Toxic chemicals, as follows:

1.

Amiton: O,O-Diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (78-53-5) and corresponding alkylated or protonated salts;

2.

PFIB: 1,1,3,3,3-Pentafluoro-2-(trifluoromethyl)-1-propene (382-21-8);

3.

SEE MILITARY GOODS CONTROLS for BZ: 3-Quinuclidinyl benzilate (6581-06-2);

4.

Phosgene: Carbonyl dichloride (75-44-5);

5.

Cyanogen chloride (506-77-4);

6.

Hydrogen cyanide (74-90-8);

7.

Chloropicrin: Trichloronitromethane (76-06-2);

Note 1: For exports to "States not Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.a.1. and .a.2. in which no individually specified chemical constitutes more than 1 % by the weight of the mixture.
Note 2: For exports to "States Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.a.1. and .a.2. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.
Note 3: 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.a.4., .a.5., .a.6. and .a.7. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.

Toxic chemical precursors, as follows:

Chemicals, other than those specified in the Military Goods Controls or in 1C350, containing a phosphorus atom to which is bonded one methyl, ethyl or propyl (normal or iso) group but not further carbon atoms;

Note 1: For exports to "States not Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 10 % by the weight of the mixture.
Note 2: For exports to "States Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.
Note 3: 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entry 1C450.b.8. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture.
Note 4: 1C450 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.
[1D] Software

[1D001] "Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 1B001 to 1B003.

[1D002] "Software" for the "development" of organic "matrix", metal "matrix" or carbon "matrix" laminates or "composites".

[1D003] "Software" specially designed or modified to enable equipment to perform the functions of equipment specified in 1A004.c. or 1A004.d.

[1D101] "Software" specially designed or modified for the operation or maintenance of goods specified in 1B101, 1B102, 1B115, 1B117, 1B118 or 1B119.

[1D103] "Software" specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.

[1D201] "Software" specially designed for the "use" of goods specified in 1B201.

[1E] Technology

[1E001] "Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 1A001.b., 1A001.c., 1A002 to 1A005, 1A006.b., 1A007, 1B or 1C.

[1E002] Other "technology" as follows:

a.

"Technology" for the "development" or "production" of polybenzothiazoles or polybenzoxazoles;

b.

"Technology" for the "development" or "production" of fluoroelastomer compounds containing at least one vinylether monomer;

c.

"Technology" for the design or "production" of the following ceramic powders or non-"composite" ceramic materials:

[1E101] "Technology" according to the General Technology Note for the "use" of goods specified in 1A102, 1B001, 1B101, 1B102, 1B115 to 1B119, 1C001, 1C101, 1C107, 1C111 to 1C118, 1D101 or 1D103.

[1E102] "Technology" according to the General Technology Note for the "development" of "software" specified in 1D001, 1D101 or 1D103.

[1E103] "Technology" for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves, when used for the "production" of "composites" or partially processed "composites".

[1E104] "Technology" relating to the "production" of pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1 573 K (1 300 °C) to 3 173 K (2 900 °C) temperature range at pressures of 130 Pa to 20 kPa.

Note: 1E104 includes "technology" for the composition of precursor gases, flow-rates and process control schedules and parameters.

[1E201] "Technology" according to the General Technology Note for the "use" of goods specified in 1A002, 1A007, 1A202, 1A225 to 1A227, 1B201, 1B225 to 1B234, 1C002.b.3. or .b.4., 1C010.b., 1C202, 1C210, 1C216, 1C225 to 1C241 or 1D201.

[1E202] "Technology" according to the General Technology Note for the "development" or "production" of goods specified in 1A007, 1A202 or 1A225 to 1A227.

[1E203] "Technology" according to the General Technology Note for the "development" of "software" specified in 1D201.

CATEGORY 2 — MATERIALS PROCESSING
[2A] Systems, Equipment and Components
N.B.: For quiet running bearings, see the Military Goods Controls.

[2A001] Anti-friction bearings and bearing systems, as follows, and components therefor:

N.B.: SEE ALSO 2A101.
Note: 2A001 does not control balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 or worse.

[2A101] Radial ball bearings, other than those specified in 2A001, having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:

a.

An inner ring bore diameter between 12 mm and 50 mm;

b.

An outer ring outside diameter between 25 mm and 100 mm; and

c.

A width between 10 mm and 20 mm.

[2A225] Crucibles made of materials resistant to liquid actinide metals, as follows:

a.

Crucibles having both of the following characteristics:

1.

A volume of between 150 cm3 and 8 000 cm3; and

2.

Made of or coated with any of the following materials, or combination of the following materials, having an overall impurity level of 2 % or less by weight:

a.

Calcium fluoride (CaF2);

b.

Calcium zirconate (metazirconate) (CaZrO3);

c.

Cerium sulphide (Ce2S3);

d.

Erbium oxide (erbia) (Er2O3);

e.

Hafnium oxide (hafnia) (HfO2);

f.

Magnesium oxide (MgO);

g.

Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W);

h.

Yttrium oxide (yttria) (Y2O3); or

i.

Zirconium oxide (zirconia) (ZrO2);

b.

Crucibles having both of the following characteristics:

1.

A volume of between 50 cm3 and 2 000 cm3; and

2.

Made of or lined with tantalum, having a purity of 99,9 % or greater by weight;

c.

Crucibles having all of the following characteristics:

1.

A volume of between 50 cm3 and 2 000 cm3;

2.

Made of or lined with tantalum, having a purity of 98 % or greater by weight; and

3.

Coated with tantalum carbide, nitride, boride, or any combination thereof.

[2A226] Valves having all of the following characteristics:

a.

A 'nominal size' of 5 mm or greater;

b.

Having a bellows seal; and

c.

Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight.

Technical Note:

For valves with different inlet and outlet diameters, the 'nominal size' in 2A226 refers to the smallest diameter.

[2B] Test, Inspection and Production Equipment
Technical Notes:
1. Secondary parallel contouring axes, (e.g., the w-axis on horizontal boring mills or a secondary rotary axis the centre line of which is parallel to the primary rotary axis) are not counted in the total number of contouring axes. Rotary axes need not rotate over 360 °. A rotary axis can be driven by a linear device (e.g., a screw or a rack-and-pinion).
2. For the purposes of 2B, the number of axes which can be co-ordinated simultaneously for "contouring control" is the number of axes along or around which, during processing of the workpiece, simultaneous and interrelated motions are performed between the workpiece and a tool. This does not include any additional axes along or around which other relative movement within the machine are performed such as:
a.

Wheel-dressing systems in grinding machines;

b.

Parallel rotary axes designed for mounting of separate workpieces;

c.

Co-linear rotary axes designed for manipulating the same workpiece by holding it in a chuck from different ends.

3. Axis nomenclature shall be in accordance with International Standard ISO 8412001, Industrial automation systems and integration - Numerical Control –of machines Coordinate system and Motion nomenclature'.
4. For the purposes of 2B001 to 2B009 a "tilting spindle" is counted as a rotary axis.
5. 'Stated "unidirectional positioning repeatability"' may be used for each machine tool model as an alternative to individual machine tests and is determined as follows:
a.

Select five machines of a model to be evaluated;

b.

Measure the linear axis repeatability (R↑,R↓) according to ISO 2302:2014 and evaluate "unidirectional positioning repeatability" for each axis of each of the five machines;

d.

Since the Category 2 list refers to each linear axis there will be as many 'stated "unidirectional positioning repeatability" values as there are linear axes;

e.

If any axis of a machine model not controlled by 2B001.a. to 2B001.c. has a 'stated "unidirectional positioning repeatability" equal to or less than the specified "unidirectional positioning repeatability" of each machine tool model plus 0,7 μm, the builder should be required to reaffirm the accuracy level once every eighteen months.

6. For the purposes of 2B001.a. to 2B001.c., measurement uncertainty for the "unidirectional positioning repeatability" of machine tools, as defined in the International Standard ISO 230/2:2014 or national equivalents, shall not be considered.
7. For the purpose of 2.B001.a. to 2B001.c.., the measurement of axes shall be made according to test procedures in 5.3.2. of ISO 230-2:2014. Tests for axes longer than 2 meters shall be made over 2 m segments. Axes longer than 4 m require multiple tests (e.g., two tests for axes longer than 4 m and up to 8 m, three tests for axes longer than 8 m and up to 12 m), each over 2 m segments and distributed in equal intervals over the axis length. Test segments are equally spaced along the full axis length, with any excess length equally divided at the beginning, in between, and at the end of the test segments. The smallest "unidirectional positioning repeatability"-value of all test segments is to be reported.

[2B001] Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or "composites", which, according to the manufacturer's technical specification, can be equipped with electronic devices for "numerical control", as follows:

N.B.: SEE ALSO 2B201.
Note 1: 2B001 does not control special purpose machine tools limited to the manufacture of gears. For such machines see 2B003.
Note 2: 2B001 does not control special purpose machine tools limited to the manufacture of any of the following:
a.

Crankshafts or camshafts;

b.

Tools or cutters;

c.

Extruder worms;

d.

Engraved or facetted jewellery parts; or

e.

Dental prostheses.

Note 3: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B001.a., b. or c.
N.B.: For optical finishing machines, see 2B002.
a.

Machine tools for turning having all of the following:

Machine tools for milling having any of the following:

Machine tools for grinding having any of the following:

[2B002] "Numerically controlled" optical finishing machine tools equipped for selective material removal to produce non-spherical optical surfaces having all of the following characteristics:

a.

Finishing the form to less (better) than 1,0 μm;

b.

Finishing to a roughness less (better) than 100 nm rms.

c.

Four or more axes which can be coordinated simultaneously for "contouring control"; and

d.

Using any of the following processes:

1.

Magnetorheological finishing ('MRF');

2.

Electrorheological finishing ('ERF');

3.

'Energetic particle beam finishing';

4.

'Inflatable membrane tool finishing'; or

5.

'Fluid jet finishing'.

Technical Notes:

For the purposes of 2B002:

1.

'MRF' is a material removal process using an abrasive magnetic fluid whose viscosity is controlled by a magnetic field.

2.

'ERF' is a removal process using an abrasive fluid whose viscosity is controlled by an electric field.

3.

'Energetic particle beam finishing' uses Reactive Atom Plasmas (RAP) or ion-beams to selectively remove material.

4.

'Inflatable membrane tool finishing' is a process that uses a pressurized membrane that deforms to contact the workpiece over a small area.

5.

'Fluid jet finishing' makes use of a fluid stream for material removal.

[2B003] "Numerically controlled" or manual machine tools, and specially designed components, controls and accessories therefor, specially designed for the shaving, finishing, grinding or honing of hardened (Rc = 40 or more) spur, helical and double-helical gears with a pitch diameter exceeding 1,250 mm and a face width of 15 % of pitch diameter or larger finished to a quality of AGMA 14 or better (equivalent to ISO 1328 class 3).

[2B004] Hot "isostatic presses" having all of the following, and specially designed components and accessories therefor:

N.B.: SEE ALSO 2B104 and 2B204.
a.

A controlled thermal environment within the closed cavity and a chamber cavity with an inside diameter of 406 mm or more; and

b.

Having any of the following:

1.

A maximum working pressure exceeding 207 MPa;

2.

A controlled thermal environment exceeding 1 773 K (1 500 °C); or

3.

A facility for hydrocarbon impregnation and removal of resultant gaseous degradation products.

Technical Note:

The inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.

N.B.: For specially designed dies, moulds and tooling see 1B003, 9B009 and the Military Goods Controls.

[2B005] Equipment specially designed for the deposition, processing and in-process control of inorganic overlays, coatings and surface modifications, as follows, for non-electronic substrates, by processes shown in the Table and associated Notes following 2E003.f., and specially designed automated handling, positioning, manipulation and control components therefor:

a.

Chemical vapour deposition (CVD) production equipment having all of the following:

Note: 2B005 does not control chemical vapour deposition, cathodic arc, sputter deposition, ion plating or ion implantation equipment, specially designed for cutting or machining tools.

[2B006] Dimensional inspection or measuring systems, equipment and "electronic assemblies", as follows:

a.

Computer controlled or "numerically controlled" Coordinate Measuring Machines (CMM), having a three dimensional (volumetric) maximum permissible error of length measurement (E0, MPE) at any point within the operating range of the machine (i.e., within the length of axes) equal to or less (better) than (1,7 + L/1 000) μm (L is the measured length in mm), according to ISO 10360-2 (2009);

Technical Note:

The E0, MPE of the most accurate configuration of the CMM specified by the manufacturer (e.g., best of the following: probe, stylus length, motion parameters, environment) and with "all compensations available" shall be compared to the 1,7 + L/1 000 μm threshold.

Linear and angular displacement measuring instruments, as follows:

'Linear displacement' measuring instruments having any of the following:

Note: Displacement measuring "laser" interferometers are only controlled in 2B006.b.1.c.
Technical Note:

For the purpose of 2B006.b.1. 'linear displacement' means the change of distance between the measuring probe and the measured object.

a.

Non-contact type measuring systems with a "resolution" equal to or less (better) than 0,2 μm within a measuring range up to 0,2 mm;

Note: 2B006 includes machine tools, other than those specified by 2B001, that can be used as measuring machines if they meet or exceed the criteria specified for the measuring machine function.

[2B007] "Robots" having any of the following characteristics and specially designed controllers and "end-effectors" therefor:

N.B.: SEE ALSO 2B207.
a.

Capable in real time of full three-dimensional image processing or full three-dimensional 'scene analysis' to generate or modify "programmes" or to generate or modify numerical programme data;

[2B008] Assemblies or units, specially designed for machine tools, or dimensional inspection or measuring systems and equipment, as follows:

a.

Linear position feedback units having an overall "accuracy" less (better) than (800 + (600 × L/1 000)) nm (L equals the effective length in mm);

[2B009] Spin-forming machines and flow-forming machines, which, according to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control and having all of the following:

N.B.: SEE ALSO 2B109 AND 2B209.
a.

Three or more axes which can be coordinated simultaneously for "contouring control"; and

b.

A roller force more than 60 kN.

Technical Note:

For the purpose of 2B009, machines combining the function of spin-forming and flow-forming are regarded as flow-forming machines.

[2B104] "Isostatic presses", other than those specified in 2B004, having all of the following:

N.B.: SEE ALSO 2B204.
a.

Maximum working pressure of 69 MPa or greater;

b.

Designed to achieve and maintain a controlled thermal environment of 873 K (600 °C) or greater; and

c.

Possessing a chamber cavity with an inside diameter of 254 mm or greater.

[2B105] Chemical vapour deposition (CVD) furnaces, other than those specified in 2B005.a., designed or modified for the densification of carbon-carbon composites.

[2B109] Flow-forming machines, other than those specified in 2B009, and specially designed components as follows:

N.B.: SEE ALSO 2B209.
a.

Flow-forming machines having all of the following:

1.

According to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control, even when not equipped with such units; and

2.

With more than two axes which can be coordinated simultaneously for "contouring control".

b.

Specially designed components for flow-forming machines specified in 2B009 or 2B109.a.

Note: 2B109 does not control machines that are not usable in the production of propulsion components and equipment (e.g. motor cases) for systems specified in 9A005, 9A007.a. or 9A105.a.
Technical Note:

Machines combining the function of spin-forming and flow-forming are for the purpose of 2B109 regarded as flow-forming machines.

[2B116] Vibration test systems, equipment and components therefor, as follows:

Technical Note:

In 2B116, 'bare table' means a flat table, or surface, with no fixture or fittings.

[2B117] Equipment and process controls, other than those specified in 2B004, 2B005.a., 2B104 or 2B105, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips.

[2B119] Balancing machines and related equipment, as follows:

N.B.: SEE ALSO 2B219.

[2B120] Motion simulators or rate tables having all of the following characteristics:

a.

Two axes or more;

b.

Designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both; and

[2B121] Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in 2B120, having all the following characteristics:

a.

Two axes or more; and

b.

A positioning "accuracy" equal to or less (better) than 5 arc second.

Note: 2B121 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008.

[2B122] Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both.

Note: Centrifuges specified in 2B122 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export.

[2B201] [X1Machine tools and any combination thereof, other than those specified in 2B001, as follows, for removing or cutting metals, ceramics or "composites", which, according to the manufacturer's technical specification, can be equipped with electronic devices for simultaneous "contouring control" in two or more axes:

Technical Note:

Stated 'positioning accuracy' levels derived under the following procedures from measurements made according to ISO 230/2 (1988) (1) or national equivalents may be used for each machine tool model if provided to, and accepted by, national authorities instead of individual machine tests. Determination of 'Stated' positioning accuracy:

a.

Select five machines of a model to be evaluated;

b.

Measure the linear axis accuracies according to ISO 230/2 (1988 (1) );

c.

Determine the accuracy values (A) for each axis of each machine. The method of calculating the accuracy value is described in the ISO 230/2 (1988) (1) 1 standard;

d.

Determine the average accuracy value of each axis. This average value becomes the stated 'positioning accuracy' of each axis for the model (Âx Ây…);

e.

Since Item 2B201 refers to each linear axis, there will be as many stated 'positioning accuracy' values as there are linear axes;

f.

If any axis of a machine tool not controlled by 2B201.a., 2B201.b. or 2B201.c.. has a stated 'positioning accuracy' of 6 μm or better (less) for grinding machines, and 8 μm or better (less) for milling and turning machines, both according to ISO 230/2 (1988) (1) , then the builder should be required to reaffirm the accuracy level once every eighteen months.

a.

Machine tools for milling, having any of the following characteristics:

1.

'Positioning accuracies' with "all compensations available" equal to or less (better) than 6 μm according to ISO 230/2 (1988) (1) or national equivalents along any linear axis;

2.

Two or more contouring rotary axes; or

2B201

a. ( continued )

3.

Five or more axes which can be coordinated simultaneously for "contouring control";

Note 1: 2B201 does not control special purpose machine tools limited to the manufacture of any of the following parts:
a.

Gears;

b.

Crankshafts or camshafts;

c.

Tools or cutters;

2B201

Note 1 (continued)

d.

Extruder worms.

Note 2: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B201.a., b. or c.]

[2B204] "Isostatic presses", other than those specified in 2B004 or 2B104, and related equipment, as follows:

a.

"Isostatic presses" having both of the following characteristics:

1.

Capable of achieving a maximum working pressure of 69 MPa or greater; and

2.

A chamber cavity with an inside diameter in excess of 152 mm;

b.

Dies, moulds and controls, specially designed for "isostatic presses" specified in 2B204.a.

Technical Note:

In 2B204 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.

[2B206] Dimensional inspection machines, instruments or systems, other than those specified in 2B006, as follows:

Note 1: Machine tools that can be used as measuring machines are controlled if they meet or exceed the criteria specified for the machine tool function or the measuring machine function.
Note 2: A machine specified in 2B206 is controlled if it exceeds the control threshold anywhere within its operating range.
Technical Notes:

All parameters of measurement values in 2B206 represent plus/minus i.e., not total band.

[2B207] "Robots", "end-effectors" and control units, other than those specified in 2B007, as follows:

a.

"Robots" or "end-effectors" specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives);

b.

Control units specially designed for any of the "robots" or "end-effectors" specified in 2B207.a.

[2B209] Flow forming machines, spin forming machines capable of flow forming functions, other than those specified in 2B009 or 2B109, and mandrels, as follows:

a.

Machines having both of the following characteristics:

1.

Three or more rollers (active or guiding); and

2.

Which, according to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control;

b.

Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm.

Note: 2B209.a. includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.

[2B219] Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:

a.

Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:

1.

Swing or journal diameter greater than 75 mm;

2.

Mass capability of from 0,9 to 23 kg; and

3.

Capable of balancing speed of revolution greater than 5 000 r.p.m.;

b.

Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:

1.

Journal diameter greater than 75 mm;

2.

Mass capability of from 0,9 to 23 kg;

3.

Capable of balancing to a residual imbalance equal to or less than 0,01 kg ×mm/kg per plane; and

4.

Belt drive type.

[2B225] Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:

a.

A capability of penetrating 0,6 m or more of hot cell wall (through-the-wall operation); or

b.

A capability of bridging over the top of a hot cell wall with a thickness of 0,6 m or more (over-the-wall operation).

Technical Note:

Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of 'master/slave' type or operated by joystick or keypad.

[2B226] Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:

N.B: SEE ALSO 3B.
a.

Furnaces having all of the following characteristics:

1.

Capable of operation above 1,123 K (850 °C);

2.

Induction coils 600 mm or less in diameter; and

3.

Designed for power inputs of 5 kW or more;

b.

Power supplies, with a specified power output of 5 kW or more, specially designed for furnaces specified in 2B226.a.

Note: 2B226.a. does not control furnaces designed for the processing of semiconductor wafers.

[2B227] Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment as follows:

a.

Arc remelt and casting furnaces having both of the following characteristics:

1.

Consumable electrode capacities between 1 000 cm3 and 20 000 cm3; and

2.

Capable of operating with melting temperatures above 1 973 K (1 700 °C);

b.

Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics:

1.

A power of 50 kW or greater; and

2.

Capable of operating with melting temperatures above 1 473 K (1,200 °C).

c.

Computer control and monitoring systems specially configured for any of the furnaces specified in 2B227.a. or b.

[2B228] Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:

a.

Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;

[2B230] All types of 'pressure transducers' capable of measuring absolute pressures and having all of the following:

a.

Pressure sensing elements made of or protected by aluminium, aluminium alloy, aluminum oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers;

b.

Seals, if any, essential for sealing the pressure sensing element, and in direct contact with the process medium, made of or protected by aluminium, aluminium alloy, aluminum oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers; and

c.

Having either of the following characteristics:

1.

A full scale of less than 13 kPa and an 'accuracy' of better than ± 1 % of full-scale; or

2.

A full scale of 13 kPa or greater and an 'accuracy' of better than ± 130 Pa when measured at 13 kPa.

Technical Notes:
1.

In 2B230 'pressure transducer' means a device that converts a pressure measurement into a signal.

2.

For the purposes of 2B230, 'accuracy' includes non-linearity, hysteresis and repeatability at ambient temperature.

[2B231] Vacuum pumps having all of the following characteristics:

a.

Input throat size equal to or greater than 380 mm;

b.

Pumping speed equal to or greater than 15 m3/s; and

c.

Capable of producing an ultimate vacuum better than 13 mPa.

Technical Notes:
1. The pumping speed is determined at the measurement point with nitrogen gas or air.
2. The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off.

[2B232] High-velocity gun systems (propellant, gas, coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 1,5 km/s or greater.

N.B.: SEE ALSO MILTARY GOODS CONTROLS.

[2B233] Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following:

N.B.: SEE ALSO 2B350.i.
a.

Capable of an inlet volume flow rate of 50 m3/h or greater;

b.

Capable of a pressure ratio of 2:1 or greater; and

c.

Having all surfaces that come in contact with the process gas made from any of the following materials:

1.

Aluminium or aluminium alloy;

2.

Aluminium oxide;

3.

Stainless steel;

4.

Nickel or nickel alloy;

5.

Phosphor bronze; or

6.

Fluoropolymers.

[2B350] Chemical manufacturing facilities, equipment and components, as follows:

a.

Reaction vessels or reactors, with or without agitators, with total internal (geometric) volume greater than 0,1 m3 (100 litres) and less than 20 m3 (20 000 litres), where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

1.

'Alloys' with more than 25 % nickel and 20 % chromium by weight;

2.

Fluoropolymers (polymeric or elastomeric materials with more than 35 % fluorine by weight);

3.

Glass (including vitrified or enamelled coating or glass lining);

4.

Nickel or 'alloys' with more than 40 % nickel by weight;

5.

Tantalum or tantalum 'alloys';

6.

Titanium or titanium 'alloys';

7.

Zirconium or zirconium 'alloys'; or

8.

Niobium (columbium) or niobium 'alloys';

b.

Agitators designed for use in reaction vessels or reactors specified in 2B350.a.; and impellers, blades or shafts designed for such agitators, where all surfaces of the agitator that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

1.

'Alloys' with more than 25 % nickel and 20 % chromium by weight;

2.

Fluoropolymers (polymeric or elastomeric materials with more than 35 % fluorine by weight);

3.

Glass (including vitrified or enamelled coatings or glass lining);

4.

Nickel or 'alloys' with more than 40 % nickel by weight;

5.

Tantalum or tantalum 'alloys';

6.

Titanium or titanium 'alloys';

7.

Zirconium or zirconium 'alloys'; or

8.

Niobium (columbium) or niobium 'alloys';

c.

Storage tanks, containers or receivers with a total internal (geometric) volume greater than 0,1 m3 (100 litres) where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

1.

'Alloys' with more than 25 % nickel and 20 % chromium by weight;

2.

Fluoropolymers (polymeric or elastomeric materials with more than 35 % fluorine by weight);

3.

Glass (including vitrified or enamelled coatings or glass lining);

4.

Nickel or 'alloys' with more than 40 % nickel by weight;

5.

Tantalum or tantalum 'alloys';

6.

Titanium or titanium 'alloys';

7.

Zirconium or zirconium 'alloys'; or

8.

Niobium (columbium) or niobium 'alloys';

d.

Heat exchangers or condensers with a heat transfer surface area greater than 0,15 m2, and less than 20 m2; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

1.

'Alloys' with more than 25 % nickel and 20 % chromium by weight;

2.

Fluoropolymers (polymeric or elastomeric materials with more than 35 % fluorine by weight);

3.

Glass (including vitrified or enamelled coatings or glass lining);

4.

Graphite or 'carbon graphite';

5.

Nickel or 'alloys' with more than 40 % nickel by weight;

6.

Tantalum or tantalum 'alloys';

7.

Titanium or titanium 'alloys';

8.

Zirconium or zirconium 'alloys';

9.

Silicon carbide;

10.

Titanium carbide; or

11.

Niobium (columbium) or niobium 'alloys';

e.

Distillation or absorption columns of internal diameter greater than 0,1 m; and liquid distributors, vapour distributors or liquid collectors designed for such distillation or absorption columns, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

1.

'Alloys' with more than 25 % nickel and 20 % chromium by weight;

2.

Fluoropolymers (polymeric or elastomeric materials with more than 35 % fluorine by weight);

3.

Glass (including vitrified or enamelled coatings or glass lining);

4.

Graphite or 'carbon graphite';

5.

Nickel or 'alloys' with more than 40 % nickel by weight;

6.

Tantalum or tantalum 'alloys';

7.

Titanium or titanium 'alloys';

8.

Zirconium or zirconium 'alloys'; or

9.

Niobium (columbium) or niobium 'alloys';

f.

Remotely operated filling equipment in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

1.

'Alloys' with more than 25 % nickel and 20 % chromium by weight; or

2.

Nickel or 'alloys' with more than 40 % nickel by weight;

g.

Valves and components, as follows:

1.

Valves, having both of the following:

a.

A 'nominal size' greater than 10 mm (3/8″); and

b.

All surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from 'corrosion resistant materials';

2.

Valves, other than those specified in 2B350.g.1., having all of the following;

a.

A 'nominal size' equal to or greater than 25,4 mm (1″) and equal to or less than 101,6 mm (4″);

b.

Casings (valve bodies) or preformed casing liners;

c.

A closure element designed to be interchangeable; and

d.

All surfaces of the casing (valve body) or preformed case liner that come in direct contact with the chemical(s) being produced, processed, or contained are made from 'corrosion resistant materials';

3.

Components, designed for valves specified in 2B350.g.1 or 2B350.g.2., in which all surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from 'corrosion resistant materials', as follows:

a.

Casings (valve bodies);

b.

Preformed casing liners;

Multiple-seal and seal-less pumps, with manufacturer's specified maximum flow-rate greater than 0,6 m3/hour, or vacuum pumps with manufacturer's specified maximum flow-rate greater than 5 m3/hour (under standard temperature (273 K (0 °C)) and pressure (101,3 kPa) conditions), other than those specified in 2B233; and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

Note: For the purposes of 2B350, the materials used for gaskets, packing, seals, screws, washers or other materials performing a sealing function do not determine the status of control, provided that such components are designed to be interchangeable.
Technical Notes:
1. 'Carbon graphite' is a composition consisting of amorphous carbon and graphite, in which the graphite content is eight percent or more by weight.
2. For the listed materials in the above entries, the term 'alloy' when not accompanied by a specific elemental concentration is understood as identifying those alloys where the identified metal is present in a higher percentage by weight than any other element.

[2B351] Toxic gas monitoring systems and their dedicated detecting components, other than those specified in 1A004, as follows; and detectors; sensor devices; and replaceable sensor cartridges therefor:

a.

Designed for continuous operation and usable for the detection of chemical warfare agents or chemicals specified in 1C350, at concentrations of less than 0,3 mg/m3; or

b.

Designed for the detection of cholinesterase-inhibiting activity.

[2B352] Equipment capable of use in handling biological materials, as follows:

a.

Complete biological containment facilities at P3, P4 containment level;

Fermenters and components as follows:

Centrifugal separators, capable of continuous separation without the propagation of aerosols, having all the following characteristics:

Cross (tangential) flow filtration equipment and components as follows:

[2C] Materials

None.

[2D] Software

[2D001] "Software", other than that specified in 2D002, as follows:

a.

"Software" specially designed or modified for the "development" or "production" of equipment specified in 2A001 or 2B001

b.

"Software" specially designed or modified for the "use" of equipment specified in 2A001.c, 2B001 or 2B003 to 2B009.

Note: 2D001 does not control part programming "software" that generates "numerical control" codes for machining various parts.

[2D002] "Software" for electronic devices, even when residing in an electronic device or system, enabling such devices or systems to function as a "numerical control" unit, capable of co-ordinating simultaneously more than four axes for "contouring control".

Note 1: 2D002 does not control "software" specially designed or modified for the operation of items not specified in Category 2.
Note 2: 2D002 does not control "software" for items specified in 2B002. See 2D001 and 2D003 for "software" for items specified in 2B002.
Note 3: 2D002 does not control "software" that is exported with, and the minimum necessary for the operation of, items not specified by Category 2.

[2D003] "Software", designed or modified for the operation of equipment specified in 2B002, that converts optical design, workpiece measurements and material removal functions into "numerical control" commands to achieve the desired workpiece form.

[2D101] "Software" specially designed or modified for the "use" of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122.

N.B.: SEE ALSO 9D004.

[2D201] "Software" specially designed for the "use" of equipment specified in 2B204, 2B206, 2B207, 2B209, 2B219 or 2B227.

[2D202] "Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 2B201.

Note: 2D202 does not control part programming "software" that generates "numerical control" command codes but does not allow direct use of equipment for machining various parts.

[2D351] "Software", other than that specified in 1D003, specially designed for "use" of equipment specified in 2B351.

[2E] Technology

[2E001] "Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 2A, 2B or 2D.

Note: 2E001 includes "technology" for the integration of probe systems into coordinate measurement machines specified in 2B006.a.

[2E002] "Technology" according to the General Technology Note for the "production" of equipment specified in 2A or 2B.

[2E003] Other "technology", as follows:

a.

"Technology" for the "development" of interactive graphics as an integrated part in "numerical control" units for preparation or modification of part programmes;

b.

"Technology" for metal-working manufacturing processes, as follows:

1.

"Technology" for the design of tools, dies or fixtures specially designed for any of the following processes:

a.

"Superplastic forming";

b.

"Diffusion bonding"; or

c.

"Direct-acting hydraulic pressing";

2.

Technical data consisting of process methods or parameters as listed below used to control:

a.

"Superplastic forming" of aluminium alloys, titanium alloys or "superalloys":

1.

Surface preparation;

2.

Strain rate;

3.

Temperature;

4.

Pressure;

b.

"Diffusion bonding" of "superalloys" or titanium alloys:

1.

Surface preparation;

2.

Temperature;

3.

Pressure;

c.

"Direct-acting hydraulic pressing" of aluminium alloys or titanium alloys:

1.

Pressure;

2.

Cycle time;

d.

"Hot isostatic densification" of titanium alloys, aluminium alloys or "superalloys":

1.

Temperature;

2.

Pressure;

3.

Cycle time;

c.

"Technology" for the "development" or "production" of hydraulic stretch-forming machines and dies therefor, for the manufacture of airframe structures;

d.

"Technology" for the "development" of generators of machine tool instructions (e.g., part programmes) from design data residing inside "numerical control" units;

e.

"Technology" for the "development" of integration "software" for incorporation of expert systems for advanced decision support of shop floor operations into "numerical control" units;

[2E101] "Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101.

[2E201] "Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 2A225, 2A226, 2B001, 2B006, 2B007.b., 2B007.c., 2B008, 2B009, 2B201, 2B204, 2B206, 2B207, 2B209, 2B225 to 2B233, 2D201 or 2D202.

[2E301] "Technology" according to the General Technology Note for the "use" of goods specified in 2B350 to 2B352.

Table

Deposition Techniques

a

The numbers in parenthesis refer to the Notes following this Table.

1. Coating Process (1)a2. Substrate3. Resultant Coating
A.Chemical Vapour Deposition (CVD)
"Superalloys"Aluminides for internal passages
Ceramics (19) and Low expansion glasses (14)

Silicides

Carbides

Dielectric layers (15)

Diamond

Diamond-like carbon (17)

Carbon-carbon, Ceramic and Metal "matrix" "composites"

Silicides

Carbides

Refractory metals

Mixtures thereof (4)

Dielectric layers (15)

Aluminides

Alloyed aluminides (2)

Boron nitride

Cemented tungsten carbide (16), Silicon carbide (18)

Carbides

Tungsten

Mixtures thereof (4)

Dielectric layers (15)

Molybdenum and Molybdenum alloysDielectric layers (15)
Beryllium and Beryllium alloys

Dielectric layers (15)

Diamond

Diamond-like carbon (17)

Sensor window materials (9)

Dielectric layers (15)

Diamond

Diamond-like carbon (17)

Thermal-Evaporation Physical Vapour Deposition (TE-PVD)
B.1.Physical Vapour Deposition (PVD): Electron-Beam (EB-PVD)
"Superalloys"

Alloyed silicides

Alloyed aluminides (2)

MCrAlX (5)

Modified zirconia (12)

Silicides

Aluminides

Mixtures thereof (4)

Ceramics (19) and Low expansion glasses (14)Dielectric layers (15)
Corrosion resistant steel (7)

MCrAlX (5)

Modified zirconia (12)

Mixtures thereof (4)

Carbon-carbon, Ceramic and Metal "matrix" "composites"

Silicides

Carbides

Refractory metals

Mixtures thereof (4)

Dielectric layers (15)

Boron nitride

Cemented tungsten carbide (16), Silicon carbide (18)

Carbides

Tungsten

Mixtures thereof (4)

Dielectric layers (15)

Molybdenum and Molybdenum alloysDielectric layers (15)
Beryllium and Beryllium alloys

Dielectric layers (15)

Borides

Beryllium

Sensor window materials (9)Dielectric layers (15)
Titanium alloys (13)

Borides

Nitrides

B.2.Ion assisted resistive heating Physical Vapour Deposition (PVD) (Ion Plating)
Ceramics (19) and Low-expansion glasses

Dielectric layers (15)

Diamond-like carbon (17)

Carbon-carbon, Ceramic and Metal "matrix" "composites"Dielectric layers (15)
Cemented tungsten carbide (16), Silicon carbideDielectric layers (15)
Molybdenum and Molybdenum alloysDielectric layers (15)
Beryllium and Beryllium alloysDielectric layers (15)
Sensor window materials (9)

Dielectric layers (15)

Diamond-like carbon (17)

B.3.Physical Vapour Deposition (PVD): "Laser" Vaporization
Ceramics (19) and Low expansion glasses (14)

Silicides

Dielectric layers (15)

Diamond-like carbon (17)

Carbon-carbon, Ceramic and Metal "matrix" "composites"Dielectric layers (15)
Cemented tungsten carbide (16), Silicon carbideDielectric layers (15)
Molybdenum and Molybdenum alloysDielectric layers (15)
Beryllium and Beryllium alloysDielectric layers (15)
Sensor window materials (9)

Dielectric layers (15)

Diamond-like carbon

B.4.Physical Vapour Deposition (PVD): Cathodic Arc Discharge
"Superalloys"

Alloyed silicides

Alloyed aluminides (2)

MCrAlX (5)

Polymers (11) and Organic "matrix" "composites"

Borides

Carbides

Nitrides

Diamond-like carbon (17)

C.Pack cementation (see A above for out-of-pack cementation) (10)
Carbon-carbon, Ceramic and Metal "matrix" "composites"

Silicides

Carbides

Mixtures thereof (4)

Titanium alloys (13)

Silicides

Aluminides

Alloyed aluminides (2)

Refractory metals and alloys (8)

Silicides

Oxides

D.Plasma spraying
"Superalloys"

MCrAlX (5)

Modified zirconia (12)

Mixtures thereof (4)

Abradable Nickel-Graphite

Abradable materials containing Ni-Cr-Al

Abradable Al-Si-Polyester

Alloyed aluminides (2)

Aluminium alloys (6)

MCrAlX (5)

Modified zirconia (12)

Silicides

Mixtures thereof (4)

Refractory metals and alloys (8)

Aluminides

Silicides

Carbides

Corrosion resistant steel (7)

MCrAlX (5)

Modified zirconia (12)

Mixtures thereof (4)

Titanium alloys (13)

Carbides

Aluminides

Silicides

Alloyed aluminides (2)

Abradable Nickel-Graphite

Abradable materials containing Ni-Cr-Al

Abradable Al-Si-Polyester

E.Slurry Deposition
Refractory metals and alloys (8)

Fused silicides

Fused aluminides except for resistance heating elements

Carbon-carbon, Ceramic and Metal "matrix" "composites"

Silicides

Carbides

Mixtures thereof (4)

F.Sputter Deposition
"Superalloys"

Alloyed silicides

Alloyed aluminides (2)

Noble metal modified aluminides (3)

MCrAlX (5)

Modified zirconia (12)

Platinum

Mixtures thereof (4)

Ceramics and Low-expansion glasses (14)

Silicides

Platinum

Mixtures thereof (4)

Dielectic layers (15)

Diamond-like carbon (17)

Titanium alloys (13)

Borides

Nitrides

Oxides

Silicides

Aluminides

Alloyed aluminides (2)

Carbides

Carbon-carbon, Ceramic and Metal "matrix" "composites"

Silicides

Carbides

Refractory metals

Mixtures thereof (4)

Dielectric layers (15)

Boron nitride

Cemented tungsten carbide (16), Silicon carbide (18)

Carbides

Tungsten

Mixtures thereof (4)

Dielectric layers (15)

Boron nitride

Molybdenum and Molybdenum alloysDielectric layers (15)
Beryllium and Beryllium alloys

Borides

Dielectric layers (15)

Beryllium

Sensor window materials (9)

Dielectric layers (15)

Diamond-like carbon (17)

Refractory metals and alloys (8)

Aluminides

Silicides

Oxides

Carbides

G.Ion Implantation
High temperature bearing steelsAdditions of Chromium Tantalum or Niobium (Columbium)
Titanium alloys (13)

Borides

Nitrides

Beryllium and Beryllium alloysBorides
Cemented tungsten carbide (16)

Carbides

Nitrides

TABLE — DEPOSITION TECHNIQUES — NOTES
1.

The term 'coating process' includes coating repair and refurbishing as well as original coating.

2.

The term 'alloyed aluminide coating' includes single or multiple-step coatings in which an element or elements are deposited prior to or during application of the aluminide coating, even if these elements are deposited by another coating process. It does not, however, include the multiple use of single-step pack cementation processes to achieve alloyed aluminides.

3.

The term 'noble metal modified aluminide' coating includes multiple-step coatings in which the noble metal or noble metals are laid down by some other coating process prior to application of the aluminide coating.

4.

The term 'mixtures thereof' includes infiltrated material, graded compositions, co-deposits and multilayer deposits and are obtained by one or more of the coating processes specified in the Table.

5.

'MCrAlX' refers to a coating alloy where M equals cobalt, iron, nickel or combinations thereof and X equals hafnium, yttrium, silicon, tantalum in any amount or other intentional additions over 0,01 % by weight in various proportions and combinations, except:

a.

CoCrAlY coatings which contain less than 22 % by weight of chromium, less than 7 % by weight of aluminium and less than 2 % by weight of yttrium;

b.

CoCrAlY coatings which contain 22 to 24 % by weight of chromium, 10 to 12 % by weight of aluminium and 0,5 to 0,7 % by weight of yttrium; or

c.

NiCrAlY coatings which contain 21 to 23 % by weight of chromium, 10 to 12 % by weight of aluminium and 0,9 to 1,1 % by weight of yttrium.

6.

The term 'aluminium alloys' refers to alloys having an ultimate tensile strength of 190 MPa or more measured at 293 K (20 °C).

7.

The term 'corrosion resistant steel' refers to AISI (American Iron and Steel Institute) 300 series or equivalent national standard steels.

8.

'Refractory metals and alloys' include the following metals and their alloys: niobium (columbium), molybdenum, tungsten and tantalum.

9.

'Sensor window materials', as follows: alumina, silicon, germanium, zinc sulphide, zinc selenide, gallium arsenide, diamond, gallium phosphide, sapphire and the following metal halides: sensor window materials of more than 40 mm diameter for zirconium fluoride and hafnium fluoride.

10.

"Technology" for single-step pack cementation of solid airfoils is not controlled by Category 2.

11.

'Polymers', as follows: polyimide, polyester, polysulphide, polycarbonates and polyurethanes.

12.

'Modified zirconia' refers to additions of other metal oxides (e.g., calcia, magnesia, yttria, hafnia, rare earth oxides) to zirconia in order to stabilise certain crystallographic phases and phase compositions. Thermal barrier coatings made of zirconia, modified with calcia or magnesia by mixing or fusion, are not controlled.

13.

'Titanium alloys' refers only to aerospace alloys having an ultimate tensile strength of 900 MPa or more measured at 293 K (20 °C).

14.

'Low-expansion glasses' refers to glasses which have a coefficient of thermal expansion of 1 × 10–7 K–1 or less measured at 293 K (20 °C).

15.

'Dielectric layers' are coatings constructed of multi-layers of insulator materials in which the interference properties of a design composed of materials of various refractive indices are used to reflect, transmit or absorb various wavelength bands. Dielectric layers refers to more than four dielectric layers or dielectric/metal "composite" layers.

16.

'Cemented tungsten carbide' does not include cutting and forming tool materials consisting of tungsten carbide/(cobalt, nickel), titanium carbide/(cobalt, nickel), chromium carbide/nickel-chromium and chromium carbide/nickel.

17.

"Technology" specially designed to deposit diamond-like carbon on any of the following is not controlled:

magnetic disk drives and heads, equipment for the manufacture of disposables, valves for faucets, acoustic diaphragms for speakers, engine parts for automobiles, cutting tools, punching-pressing dies, office automation equipment, microphones or medical devices or moulds, for casting or moulding of plastics, manufactured from alloys containing less than 5 % beryllium.

18.

'Silicon carbide' does not include cutting and forming tool materials.

19.

Ceramic substrates, as used in this entry, does not include ceramic materials containing 5 % by weight, or greater, clay or cement content, either as separate constituents or in combination.

TABLE — DEPOSITION TECHNIQUES — TECHNICAL NOTE

Processes specified in Column 1 of the Table are defined as follows:

a.

Chemical Vapour Deposition (CVD) is an overlay coating or surface modification coating process wherein a metal, alloy, "composite", dielectric or ceramic is deposited upon a heated substrate. Gaseous reactants are decomposed or combined in the vicinity of a substrate resulting in the deposition of the desired elemental, alloy or compound material on the substrate. Energy for this decomposition or chemical reaction process may be provided by the heat of the substrate, a glow discharge plasma, or "laser" irradiation.

N.B. 1 CVD includes the following processes: directed gas flow out-of-pack deposition, pulsating CVD, controlled nucleation thermal deposition (CNTD), plasma enhanced or plasma assisted CVD processes.
N.B. 2 Pack denotes a substrate immersed in a powder mixture.

Thermal Evaporation-Physical Vapour Deposition (TE-PVD) is an overlay coating process conducted in a vacuum with a pressure less than 0,1 Pa wherein a source of thermal energy is used to vaporize the coating material. This process results in the condensation, or deposition, of the evaporated species onto appropriately positioned substrates.

The addition of gases to the vacuum chamber during the coating process to synthesize compound coatings is an ordinary modification of the process.

The use of ion or electron beams, or plasma, to activate or assist the coating's deposition is also a common modification in this technique. The use of monitors to provide in-process measurement of optical characteristics and thickness of coatings can be a feature of these processes.

Specific TE-PVD processes are as follows:

Plasma Spraying is an overlay coating process wherein a gun (spray torch) which produces and controls a plasma accepts powder or wire coating materials, melts them and propels them towards a substrate, whereon an integrally bonded coating is formed. Plasma spraying constitutes either low pressure plasma spraying or high velocity plasma spraying.

N.B. 1 Low pressure means less than ambient atmospheric pressure.
CATEGORY 3 — ELECTRONICS
[3A] Systems, Equipment and Components
Note 1: The control status of equipment and components described in 3A001 or 3A002, other than those described in 3A001.a.3. to 3A001.a.10., 3A001.a.12. or 3A001.a.13, which are specially designed for or which have the same functional characteristics as other equipment is determined by the control status of the other equipment.
Note 2: The control status of integrated circuits described in 3A001.a.3. to 3A001.a.9., 3A001.a.12. or 3A001.a.13 Which are unalterably programmed or designed for a specific function for another equipment is determined by the control status of the other equipment.
N.B.: When the manufacturer or applicant cannot determine the control status of the other equipment, the control status of the integrated circuits is determined in 3A001.a.3. to 3A001.a.9., 3A001.a.12 and 3A001.a.13.

[3A001] Electronic components and specially designed components therefor, as follows:

a.

General purpose integrated circuits, as follows:

Note 1: The control status of wafers (finished or unfinished), in which the function has been determined, is to be evaluated against the parameters of 3A001.a.
Note 2: Integrated circuits include the following types:
  • "Monolithic integrated circuits";

  • "Hybrid integrated circuits";

  • "Multichip integrated circuits";

  • "Film type integrated circuits", including silicon-on-sapphire integrated circuits;

  • "Optical integrated circuits";

  • "Three dimensional integrated circuits".

1.

Integrated circuits designed or rated as radiation hardened to withstand any of the following:

"Microprocessor microcircuits", "microcomputer microcircuits", microcontroller microcircuits, storage integrated circuits manufactured from a compound semiconductor, analogue-to-digital converters, digital-to-analogue converters, electro-optical or "optical integrated circuits" designed for "signal processing", field programmable logic devices, custom integrated circuits for which either the function is unknown or the control status of the equipment in which the integrated circuit will be used is unknown, Fast Fourier Transform (FFT) processors, electrical erasable programmable read-only memories (EEPROMs), flash memories or static random-access memories (SRAMs), having any of the following:

"Microprocessor microcircuits", "microcomputer microcircuits" and microcontroller microcircuits, manufactured from a compound semiconductor and operating at a clock frequency exceeding 40 MHz;

Analogue-to-Digital Converter (ADC) and Digital-to-Analogue Converter (DAC) integrated circuits, as follows:

ADCs having any of the following:

N.B.: SEE ALSO 3A101
1.

A resolution of 8 bit or more, but less than 10 bit, with an output rate greater than 1,000 million words per second;

2.

A resolution of 10 bit or more, but less than 12 bit, with an output rate greater than 300 million words per second;

3.

A resolution of 12 bit with an output rate greater than 200 million words per second;

4.

A resolution of more than 12 bit, but equal to or less than 14 bit, with an output rate greater than 125 million words per second; or

5.

A resolution of more than 14 bit with an output rate greater than 20 million words per second;

Technical Notes:
1. A resolution of n bit corresponds to a quantisation of 2n levels.
2. The number of bits in the output word is equal to the resolution of the ADC.
3. The output rate is the maximum output rate of the converter, regardless of the architecture or oversampling.
4. For 'multiple channel ADCs', the outputs are not aggregated and the output rate is the maximum output rate of any single channel.
5. For 'interleaved ADCs' or for 'multiple channel ADCs' that are specified to have an interleaved mode of operation, the outputs are aggregated and the output rate is the maximum combined total output rate of all of the outputs.
6. Vendors may also refer to the output rate as sampling rate, conversion rate or throughput rate. It is often specified in megahertz (MHz) or mega samples per second (MSPS).
7. For the purpose of measuring output rate, one output word per second is equivalent to one Hertz or one sample per second.
8. 'Multiple channel ADCs' are defined as devices which integrate more than one ADC, designed so that each ADC has a separate analogue input.

Digital-to-Analogue Converters (DAC) having any of the following:

[X1A resolution of 12 bit or more with an 'adjusted update rate' of greater than 1 250 MSPS and having any of the following:]

a.

A settling time less than 9 ns to 0,024 % of full scale from a full scale step; or

b.

A 'Spurious Free Dynamic Range' (SFDR) greater than 68 dBc (carrier) when synthesising a full scale analogue signal of 100 MHz or the highest full scale analogue signal frequency specified below 100 MHz.

'Field programmable logic devices' having any of the following:

Note: 3A001.a.7. includes:
  • Simple Programmable Logic Devices (SPLDs)

  • Complex Programmable Logic Devices (CPLDs)

  • Field Programmable Gate Arrays (FPGAs)

  • Field Programmable Logic Arrays (FPLAs)

  • Field Programmable Interconnects (FPICs)

Microwave or millimetre wave components, as follows:

Technical Note:

For purposes of 3A001.b., the parameter peak saturated power output may also be referred to on product data sheets as output power, saturated power output, maximum power output, peak power output, or peak envelope power output.

1.

Electronic vacuum tubes and cathodes, as follows:

Note 1: 3A001.b.1. does not control tubes designed or rated for operation in any frequency band and having all of the following:
a.

Does not exceed 31,8 GHz; and

b.

Is "allocated by the ITU" for radio-communications services, but not for radio-determination.

Microwave "Monolithic Integrated Circuits" (MMIC) power amplifiers that are any of the following:

Note 1: Not used.
Note 2: The control status of the MMIC whose rated operating frequency includes frequencies listed in more than one frequency range, as defined by 3A001.b.2.a. to 3A001.b.2.h., is determined by the lowest peak saturated power output threshold.

Discrete microwave transistors that are any of the following:

Note 1: The control status of a transistor whose rated operating frequency includes frequencies listed in more than one frequency range, as defined by 3A001.b.3.a. to 3A001.b.3.e., is determined by the lowest peak saturated power output threshold.

Microwave solid state amplifiers and microwave assemblies/modules containing microwave solid state amplifiers, that are any of the following:

Technical Note:

2.7 GHz should be used as the lowest operating frequency (fGHz) in the formula in 3A001.b.4.f.3., for amplifiers that have a rated operating range extending downward to 2.7 GHz and below [d ≤ 15 cm*GHz/2,7 GHz].

N.B.: MMIC power amplifiers should be evaluated against the criteria in 3A001.b.2.
Note 1: Not used.
Note 2: The control status of an item whose rated operating frequency includes frequencies listed in more than one frequency range, as defined by 3A001.b.4.a. to 3A001.b.4.e., is determined by the lowest peak saturation output threshold.

Microwave power amplifiers containing tubes specified in 3A001.b.1. and having all of the following:

Microwave power modules (MPM) consisting of, at least, a travelling wave tube, a microwave "monolithic integrated circuit" and an integrated electronic power conditioner and having all of the following:

Technical Notes:
1. To calculate the volume in 3A001.b.9.b., the following example is provided: for a maximum rated power of 20 W, the volume would be: 20 W × 10 cm3/W = 200 cm3.

Acoustic wave devices as follows and specially designed components therefor:

High energy devices as follows:

'Cells' as follows:

Technical Notes:
1. For the purpose of 3A001.e.1.,'energy density' (Wh/kg) is calculated from the nominal voltage multiplied by the nominal capacity in ampere-hours (Ah) divided by the mass in kilograms. If the nominal capacity is not stated, energy density is calculated from the nominal voltage squared then multiplied by the discharge duration in hours divided by the discharge load in ohms and the mass in kilograms.
2. For the purpose of 3A001.e.1., a 'cell' is defined as an electrochemical device, which has positive and negative electrodes, an electrolyte, and is a source of electrical energy. It is the basic building block of a battery.
3. For the purpose of 3A001.e.1.a., a 'primary cell' is a 'cell' that is not designed to be charged by any other source.
4. For the purpose of 3A001.e.1.b., a 'secondary cell' is a 'cell' that is designed to be charged by an external electrical source.

High energy storage capacitors as follows:

Solid-state pulsed power switching thyristor devices and 'thyristor modules', using either electrically, optically, or electron radiation controlled switch methods and having any of the following:

Note 1: 3A001.g. includes:
  • Silicon Controlled Rectifiers (SCRs)

  • Electrical Triggering Thyristors (ETTs)

  • Light Triggering Thyristors (LTTs)

  • Integrated Gate Commutated Thyristors (IGCTs)

  • Gate Turn-off Thyristors (GTOs)

  • MOS Controlled Thyristors (MCTs)

  • Solidtrons

Note 2: 3A001.g. does not control thyristor devices and 'thyristor modules' incorporated into equipment designed for civil railway or "civil aircraft" applications.

Solid-state power semiconductor switches, diodes, or 'modules', having all of the following:

Note 1: Repetitive peak off-state voltage in 3A001.h. includes drain to source voltage, collector to emitter voltage, repetitive peak reverse voltage and peak repetitive off-state blocking voltage.

[3A002] General purpose electronic equipment as follows:

a.

Recording equipment and oscilloscopes as follows:

1.

Not used;

2.

Not used;

3.

Not used;

4.

Not used;

5.

Waveform digitisers and transient recorders, having all of the following:

"Signal analysers" as follows:

Signal generators having any of the following:

Single sideband (SSB) phase noise, in dBc/Hz, specified as being any of the following:

A maximum frequency exceeding 90 GHz;

[3A003] Spray cooling thermal management systems employing closed loop fluid handling and reconditioning equipment in a sealed enclosure where a dielectric fluid is sprayed onto electronic components using specially designed spray nozzles that are designed to maintain electronic components within their operating temperature range, and specially designed components therefor.

[3A101] Electronic equipment, devices and components, other than those specified in 3A001, as follows:

a.

Analogue-to-digital converters, usable in "missiles", designed to meet military specifications for ruggedized equipment;

b.

Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and systems containing those accelerators.

Note: 3A101.b. above does not specify equipment specially designed for medical purposes.

[3A102] 'Thermal batteries' designed or modified for 'missiles'.

Technical Notes:
1. In 3A102 'thermal batteries' are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery.
2. In 3A102 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[3A201] Electronic components, other than those specified in 3A001, as follows;

a.

Capacitors having either of the following sets of characteristics:

1.
a.

Voltage rating greater than 1,4 kV;

b.

Energy storage greater than 10 J;

c.

Capacitance greater than 0,5 μF; and

d.

Series inductance less than 50 nH; or

2.
a.

Voltage rating greater than 750 V;

b.

Capacitance greater than 0,25 μF; and

c.

Series inductance less than 10 nH;

b.

Superconducting solenoidal electromagnets having all of the following characteristics:

1.

Capable of creating magnetic fields greater than 2 T;

2.

A ratio of length to inner diameter greater than 2;

3.

Inner diameter greater than 300 mm; and

4.

Magnetic field uniform to better than 1 % over the central 50 % of the inner volume;

Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:

Note: 3A201.c. does not control accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes:
Technical Notes:
1. The 'figure of merit' K is defined as:

K = 1,7 × 103V2.65Q

V is the peak electron energy in million electron volts.

If the accelerator beam pulse duration is less than or equal to 1 μs, then Q is the total accelerated charge in Coulombs. If the accelerator beam pulse duration is greater than 1 μs, then Q is the maximum accelerated charge in 1 μs.

Q equals the integral of i with respect to t, over the lesser of 1 μs or the time duration of the beam pulse (Q = ∫ idt), where i is beam current in amperes and t is time in seconds.

[3A225] Frequency changers or generators, other than those specified in 0B001.b.13., usable as a variable or fixed frequency motor drive, having all of the following characteristics:

N.B. 1: "Software" specially designed to enhance or release the performance of a frequency changer or generator to meet the characteristics of 3A225 is specified in 3D225.
N.B. 2: "Technology" in the form of codes or keys to enhance or release the performance of a frequency changer or generator to meet the characteristics of 3A225 is specified in 3E225.
a.

Multiphase output providing a power of 40 VA or greater;

b.

Operating at a frequency of 600 Hz or more; and

c.

Frequency control better (less) than 0,2 %.

[3A226] High-power direct current power supplies, other than those specified in 0B001.j.6., having both of the following characteristics:

a.

Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; and

b.

Current or voltage stability better than 0,1 % over a time period of 8 hours.

[3A227] High-voltage direct current power supplies, other than those specified in 0B001.j.5., having both of the following characteristics:

a.

Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; and

b.

Current or voltage stability better than 0,1 % over a time period of 8 hours.

[3A228] Switching devices, as follows:

[3A229] High-current pulse generators as follows:

N.B.: SEE ALSO MILITARY GOODS CONTROLS.

[3A230] High-speed pulse generators, and 'pulse heads' therefor, having both of the following characteristics:

a.

Output voltage greater than 6 V into a resistive load of less than 55 ohms, and

b.

'Pulse transition time' less than 500 ps.

Technical Notes:
1. In 3A230, 'pulse transition time' is defined as the time interval between 10 % and 90 % voltage amplitude.
2. 'Pulse heads' are impulse forming networks designed to accept a voltage step function and shape it into a variety of pulse forms that can include rectangular, triangular, step, impulse, exponential, or monocycle types. 'Pulse heads' can be an integral part of the pulse generator, they can be a plug-in module to the device or they can be an externally connected device.

[3A231] Neutron generator systems, including tubes, having both of the following characteristics:

a.

Designed for operation without an external vacuum system; and

b.

Utilizing any of the following:

1.

Electrostatic acceleration to induce a tritium-deuterium nuclear reaction; or

2.

Electrostatic acceleration to induce a deuterium-deuterium nuclear reaction and capable of an output of 3 × 109 neutrons/s or greater.

[3A232] Multipoint initiation systems, other than those specified in 1A007, as follows:

N.B.: SEE ALSO MILITARY GOODS CONTROLS.
N.B.: See 1A007.b. for detonators.
a.

Not used;

b.

Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over greater than 5,000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2,5 μs.

Note: 3A232 does not control detonators using only primary explosives, such as lead azide.

[3A233] Mass spectrometers, other than those specified in 0B002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:

a.

Inductively coupled plasma mass spectrometers (ICP/MS);

b.

Glow discharge mass spectrometers (GDMS);

c.

Thermal ionization mass spectrometers (TIMS);

d.

Electron bombardment mass spectrometers having both of the following features:

1.

A molecular beam inlet system that injects a collimated beam of analyte molecules into a region of the ion source where the molecules are ionized by an electron beam; and

2.

One or more 'cold traps' that can be cooled to a temperature of 193 K (– 80 °C);

e.

Not used;

f.

Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.

Technical Notes:
1. Electron bombardment mass spectrometers in 3A233.d. are also known as electron impact mass spectrometers or electron ionization mass spectrometers.
2. In 3A233.d.2., a 'cold trap' is a device that traps gas molecules by condensing or freezing them on cold surfaces. For the purposes of 3A233.d.2., a closed-loop gaseous helium cryogenic vacuum pump is not a 'cold trap'.

[3A234] Striplines to provide low inductance path to detonators with the following characteristics:

a.

Voltage rating greater than 2 kV; and

b.

Inductance of less than 20 nH.

[3B] Test, Inspection and Production Equipment

[3B001] Equipment for the manufacturing of semiconductor devices or materials, as follows and specially designed components and accessories therefor:

a.

Equipment designed for epitaxial growth as follows:

Automatic loading multi-chamber central wafer handling systems having all of the following:

Note: 3B001.e. does not control automatic robotic wafer handling systems specially designed for parallel wafer processing.
Technical Notes:
1. For the purpose of 3B001.e., 'semiconductor process tools' refers to modular tools that provide physical processes for semiconductor production that are functionally different, such as deposition, etch, implant or thermal processing.

Lithography equipment as follows:

[3B002] Test equipment specially designed for testing finished or unfinished semiconductor devices as follows and specially designed components and accessories therefor:

a.

For testing S-parameters of transistor devices at frequencies exceeding 31,8 GHz;

b.

Not used;

c.

For testing microwave integrated circuits specified in 3A001.b.2.

[3C] Materials

[3C001] Hetero-epitaxial materials consisting of a "substrate" having stacked epitaxially grown multiple layers of any of the following:

a.

Silicon (Si);

b.

Germanium (Ge);

c.

Silicon carbide (SiC); or

d.

"III/V compounds" of gallium or indium.

Note: 3C001.d. does not control a "substrate" having one or more P-type epitaxial layers of GaN, InGaN, AlGaN, InAlN, InAlGaN, GaP, InGaP, AlInP or InGaAlP, independent of the sequence of the elements, except if the P-type epitaxial layer is between N-type layers.

[3C002] Resist materials as follows and "substrates" coated with the following resists:

a.

Resists designed for semiconductor lithography as follows:

1.

Positive resists adjusted (optimised) for use at wavelengths less than 245 nm but equal to or greater than 15 nm;

2.

Resists adjusted (optimised) for use at wavelengths less than 15 nm but greater than 1 nm;

b.

All resists designed for use with electron beams or ion beams, with a sensitivity of 0,01 μcoulomb/mm2 or better;

c.

Not used;

d.

All resists optimised for surface imaging technologies;

e.

All resists designed or optimised for use with imprint lithography equipment specified in 3B001.f.2. that use either a thermal or photo-curable process.

[3C003] Organo-inorganic compounds as follows:

a.

Organo-metallic compounds of aluminium, gallium or indium, having a purity (metal basis) better than 99,999 %;

b.

Organo-arsenic, organo-antimony and organo-phosphorus compounds, having a purity (inorganic element basis) better than 99,999 %.

Note: 3C003 only controls compounds whose metallic, partly metallic or non-metallic element is directly linked to carbon in the organic part of the molecule.

[3C004] Hydrides of phosphorus, arsenic or antimony, having a purity better than 99,999 %, even diluted in inert gases or hydrogen.

Note: 3C004 does not control hydrides containing 20 % molar or more of inert gases or hydrogen.

[3C005] Silicon carbide (SiC), gallium nitride (GaN), aluminium nitride (AlN) or aluminium gallium nitride (AlGaN) semiconductor "substrates", or ingots, boules, or other preforms of those materials, having resistivities greater than 10 000 ohm-cm at 20 °C.

[3C006] "Substrates" specified in 3C005 With at least one epitaxial layer of silicon carbide, gallium nitride, aluminium nitride or aluminium gallium nitride.

[3D] Software

[3D001] "Software" specially designed for the "development" or "production" of equipment specified in 3A001.b. to 3A002.g. or 3B.

[3D002] "Software" specially designed for the "use" of equipment specified in 3B001.a. to f., 3B002 or 3A225

[3D003] 'Physics-based' simulation "software" specially designed for the "development" of lithographic, etching or deposition processes for translating masking patterns into specific topographical patterns in conductors, dielectrics or semiconductor materials.

Technical Note:

'Physics-based' in 3D003 means using computations to determine a sequence of physical cause and effect events based on physical properties (e.g., temperature, pressure, diffusion constants and semiconductor materials properties).

Note: Libraries, design attributes or associated data for the design of semiconductor devices or integrated circuits are considered as "technology".

[3D004] "Software" specially designed for the "development" of the equipment specified in 3A003.

[3D101] "Software" specially designed or modified for the "use" of equipment specified in 3A101.b.

[3D225] "Software" specially designed to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225.

[3E] Technology

[3E001] "Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 3A, 3B or 3C;

Note 1: 3E001 does not control "technology" for the "production" of equipment or components controlled by 3A003.
Note 2: 3E001 does not control "technology" for the "development" or "production" of integrated circuits specified in 3A001.a.3. to 3A001.a.12., having all of the following:
a.

Using "technology" at or above 0.130 μm; and

b.

Incorporating multi-layer structures with three or fewer metal layers.

[3E002] "Technology" according to the General Technology Note, other than that specified in 3E001, for the "development" or "production" of a "microprocessor microcircuit", "microcomputer microcircuit" or microcontroller microcircuit core, having an arithmetic logic unit with an access width of 32 bits or more and any of the following features or characteristics:

Note 1: 3E002 does not control "technology" for the "development" or "production" of micro-processor cores, having all of the following:
a.

Using "technology" at or above 0.130 μm; and

b.

Incorporating multi-layer structures with five or fewer metal layers.

Note 2: 3E002 includes "technology" for digital signal processors and digital array processors.

[3E003] Other "technology" for the "development" or "production" of the following:

[3E101] "Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 3A001.a.1. or 2., 3A101, 3A102 or 3D101.

[3E102] "Technology" according to the General Technology Note for the "development" of "software" specified in 3D101.

[3E201] "Technology" according to the General Technology Note for the "use" of equipment specified in 3A001.e.2., 3A001.e.3., 3A001.g., 3A201, 3A225 to 3A234.

[3E225] "Technology", in the form of codes or keys, to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225.

CATEGORY 4 — COMPUTERS
Note 1: Computers, related equipment and "software" performing telecommunications or "local area network" functions must also be evaluated against the performance characteristics of Category 5, Part 1 (Telecommunications).
Note 2: Control units which directly interconnect the buses or channels of central processing units, "main storage" or disk controllers are not regarded as telecommunications equipment described in Category 5, Part 1 (Telecommunications).
N.B.: For the control status of "software" specially designed for packet switching, see 5D001.
Note 3: Computers, related equipment and "software" performing cryptographic, cryptanalytic, certifiable multi-level security or certifiable user isolation functions, or which limit electromagnetic compatibility (EMC), must also be evaluated against the performance characteristics in Category 5, Part 2 ("Information Security").
[4A] Systems, Equipment and Components

[4A001] Electronic computers and related equipment, having any of the following and "electronic assemblies" and specially designed components therefor:

N.B.: SEE ALSO 4A101.

[4A003] "Digital computers", "electronic assemblies", and related equipment therefor, as follows and specially designed components therefor:

Note 1: 4A003 includes the following:
  • 'Vector processors';

  • Array processors;

  • Digital signal processors;

  • Logic processors;

  • Equipment designed for "image enhancement";

  • Equipment designed for "signal processing".

Note 2: The control status of the "digital computers" and related equipment described in 4A003 is determined by the control status of other equipment or systems provided:
a.

The "digital computers" or related equipment are essential for the operation of the other equipment or systems;

a.

Not used;

b.

"Digital computers" having an "Adjusted Peak Performance" ("APP") exceeding 8.0 weighted TeraFLOPS (WT);

c.

"Electronic assemblies" specially designed or modified for enhancing performance by aggregation of processors so that the "APP" of the aggregation exceeds the limit specified in 4A003.b.;

[4A004] Computers as follows and specially designed related equipment, "electronic assemblies" and components therefor:

a.

"Systolic array computers";

b.

"Neural computers";

c.

"Optical computers".

[4A005] Systems, equipment, and components therefor, specially designed or modified for the generation, operation or delivery of, or communication with, "intrusion software".

[4A101] Analogue computers, "digital computers" or digital differential analysers, other than those specified in 4A001.a.1., which are ruggedized and designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

[4A102] "Hybrid computers" specially designed for modelling, simulation or design integration of space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

Note: This control only applies when the equipment is supplied with "software" specified in 7D103 or 9D103.
[4B] Test, Inspection and Production Equipment

None.

[4C] Materials

None.

[4D] Software
Note: The control status of "software" for equipment described in other Categories is dealt with in the appropriate Category.

[4D001] "Software" as follows:

a.

"Software" specially designed or modified for the "development" or "production" of equipment or "software" specified in 4A001 to 4A004, or 4D.

b.

"Software", other than that specified in 4D001.a., specially designed or modified for the "development" or "production" of equipment as follows:

1.

"Digital computers" having an "Adjusted Peak Performance" ("APP") exceeding 1,0 weighted TeraFLOPS (WT);

2.

"Electronic assemblies" specially designed or modified for enhancing performance by aggregation of processors so that the "APP" of the aggregation exceeds the limit in 4D001.b.1.

[4D002] Not used

[4D003] Not used.

[4D004] "Software" specially designed or modified for the generation, operation or delivery of, or communication with, "intrusion software".

[4E] Technology

[4E001]

a.

"Technology" according to the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 4A or 4D.

b.

"Technology", other than that specified in 4E001.a., specially designed or modified for the "development" or "production" of equipment as follows:

1.

"Digital computers" having an "Adjusted Peak Performance" ("APP") exceeding 1,0 weighted TeraFLOPS (WT);

2.

"Electronic assemblies" specially designed or modified for enhancing performance by aggregation of processors so that the "APP" of the aggregation exceeds the limit in 4E001.b.1.

c.

"Technology" for the "development" of "intrusion software".

TECHNICAL NOTE ON "ADJUSTED PEAK PERFORMANCE" ("APP")

"APP" is an adjusted peak rate at which "digital computers" perform 64-bit or larger floating point additions and multiplications.

"APP" is expressed in Weighted TeraFLOPS (WT), in units of 1012 adjusted floating point operations per second

Abbreviations used in this Technical Note
n

number of processors in the "digital computer"

i

processor number (i,…n)

ti

processor cycle time (ti = 1/Fi)

Fi

processor frequency

Ri

peak floating point calculating rate

Wi

architecture adjustment factor

Outline of "APP" calculation method
1.For each processor i, determine the peak number of 64-bit or larger floating point operations, FPOi, performed per cycle for each processor in the "digital computer".
Note In determining FPO, include only 64-bit or larger floating point additions and/or multiplications. All floating point operations must be expressed in operations per processor cycle; operations requiring multiple cycles may be expressed in fractional results per cycle. For processors not capable of performing calculations on floating point operands of 64-bit or more, the effective calculating rate R is zero.
2.Calculate the floating point rate R for each processor Ri = FPOi/ti.
3.Calculate "APP" as "APP" = W1 × R1 + W2 × R2 + … + Wn × Rn.
4.For 'vector processors', Wi = 0,9. For non-'vector processors', Wi = 0,3.
Note 1 For processors that perform compound operations in a cycle, such as addition and multiplication, each operation is counted.
Note 2 For a pipelined processor the effective calculating rate R is the faster of the pipelined rate, once the pipeline is full, or the non-pipelined rate.
Note 3 The calculating rate R of each contributing processor is to be calculated at its maximum value theoretically possible before the "APP" of the combination is derived. Simultaneous operations are assumed to exist when the computer manufacturer claims concurrent, parallel, or simultaneous operation or execution in a manual or brochure for the computer.
Note 4 Do not include processors that are limited to input/output and peripheral functions (e.g., disk drive, communication and video display) when calculating "APP".
Note 5 "APP" values are not to be calculated for processor combinations (inter)connected by "Local Area Networks", Wide Area Networks, I/O shared connections/devices, I/O controllers and any communication interconnection implemented by "software".
Note 6 "APP" values must be calculated for processor combinations containing processors specially designed to enhance performance by aggregation, operating simultaneously and sharing memory;
Technical Note:
1. Aggregate all processors and accelerators operating simultaneously and located on the same die.
2. Processor combinations share memory when any processor is capable of accessing any memory location in the system through the hardware transmission of cache lines or memory words, without the involvement of any software mechanism, which may be achieved using "electronic assemblies" specified in 4A003.c.
Note 7 A 'vector processor' is defined as a processor with built-in instructions that perform multiple calculations on floating-point vectors (one-dimensional arrays of 64-bit or larger numbers) simultaneously, having at least 2 vector functional units and at least 8 vector registers of at least 64 elements each.
CATEGORY 5 — TELECOMMUNICATIONS AND "INFORMATION SECURITY"
PART 1 — U.K. TELECOMMUNICATIONS
Note 1: The control status of components, "lasers", test and "production" equipment and "software", therefor which are specially designed for telecommunications equipment or systems is determined in Category 5, Part 1.
N.B. 1: For "lasers" specially designed for telecommunications equipment or systems, see 6A005.
N.B. 2: See also Category 5, Part 2 for equipment, components, and "software", performing or incorporating "information security" functions.
Note 2: "Digital computers", related equipment or "software", when essential for the operation and support of telecommunications equipment described in this Category, are regarded as specially designed components, provided they are the standard models customarily supplied by the manufacturer. This includes operation, administration, maintenance, engineering or billing computer systems.
[5A1] Systems, Equipment and Components

[5A001] Telecommunications systems, equipment, components and accessories as follows:

a.

Any type of telecommunications equipment having any of the following characteristics, functions or features:

Telecommunication systems and equipment, and specially designed components and accessories therefor, having any of the following characteristics, functions or features:

Being radio equipment employing "spread spectrum" techniques, including "frequency hopping" techniques, other than those specified in 5A001.b.4. and having any of the following:

Being digitally controlled radio receivers having all of the following:

Optical fibres of more than 500 m in length and specified by the manufacturer as being capable of withstanding a 'proof test' tensile stress of 2 × 109 N/m2 or more;

N.B.: For underwater umbilical cables, see 8A002.a.3.

"Electronically steerable phased array antennae" operating above 31,8 GHz;

Mobile telecommunications interception or jamming equipment, and monitoring equipment therefor, as follows, and specially designed components therefor:

Passive Coherent Location (PCL) systems or equipment, specially designed for detecting and tracking moving objects by measuring reflections of ambient radio frequency emissions, supplied by non-radar transmitters;

Technical Note:

Non-radar transmitters may include commercial radio, television or cellular telecommunications base stations.

Counter Improvised Explosive Device (IED) equipment and related equipment, as follows:

[5A101] Telemetry and telecontrol equipment, including ground equipment, designed or modified for 'missiles'.

Technical Note:

In 5A101 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

Note: 5A101 does not control:
a.

Equipment designed or modified for manned aircraft or satellites;

b.

Ground based equipment designed or modified for terrestrial or marine applications;

c.

Equipment designed for commercial, civil or 'Safety of Life' (e.g. data integrity, flight safety) GNSS services;

[5B1] Test, Inspection and Production Equipment

[5B001] Telecommunications test, inspection and production equipment, components and accessories, as follows:

a.

Equipment and specially designed components or accessories therefor, specially designed for the "development" or "production" of equipment, functions or features, specified in 5A001;

Equipment and specially designed components or accessories therefor, specially designed for the "development" of any of the following telecommunication transmission or switching equipment:

[5C1] Materials

None

[5D1] Software

[5D001] "Software" as follows:

[5D101] "Software" specially designed or modified for the "use" of equipment specified in 5A101.

[5E1] Technology

[5E001] "Technology" as follows:

a.

"Technology" according to the General Technology Note for the "development", "production" or "use" (excluding operation) of equipment, functions or features specified in 5A001 or "software" specified in 5D001.a.;

b.

Specific "technology" as follows:

"Technology" according to the General Technology Note for the "development" or "production" of any of the following:

Equipment employing digital techniques designed to operate at a "total digital transfer rate" exceeding 560 Gbit/s;

Equipment employing a "laser" and having any of the following:

Employing coherent optical transmission or coherent optical detection techniques;

"Technology" according to the General Technology Note for the "development" or "production" of Microwave Monolithic Integrated Circuit (MMIC) power amplifiers specially designed for telecommunications and that are any of the following:

Technical Note:

For purposes of 5E001.d., the parameter peak saturated power output may also be referred to on product data sheets as output power, saturated power output, maximum power output, peak power output, or peak envelope power output.

1.

Rated for operation at frequencies exceeding 2.7 GHz up to and including 6,8 GHz with a "fractional bandwidth" greater than 15 %, and having any of the following:

a.

A peak saturated power output greater than 75 W (48,75 dBm) at any frequency exceeding 2,7 GHz up to and including 2,9 GHz;

b.

A peak saturated power output greater than 55 W (47,4 dBm) at any frequency exceeding 2,9 GHz up to and including 3,2 GHz;

c.

A peak saturated power output greater than 40 W (46 dBm) at any frequency exceeding 3,2 GHz up to and including 3,7 GHz; or

d.

A peak saturated power output greater than 20 W (43 dBm) at any frequency exceeding 3,7 GHz up to and including 6,8 GHz;

2.

Rated for operation at frequencies exceeding 6,8 GHz up to and including 16 GHz with a "fractional bandwidth" greater than 10 %, and having any of the following:

a.

A peak saturated power output greater than 10 W (40 dBm) at any frequency exceeding 6,8 GHz up to and including 8,5 GHz; or

b.

A peak saturated power output greater than 5 W (37 dBm) at any frequency exceeding 8,5 GHz up to and including 16 GHz;

3.

Rated for operation with a peak saturated power output greater than 3 W (34,77 dBm) at any frequency exceeding 16 GHz up to and including 31,8 GHz, and with a "fractional bandwidth" of greater than 10 %;

4.

Rated for operation with a peak saturated power output greater than 0,1 nW (-70 dBm) at any frequency exceeding 31,8 GHz up to and including 37 GHz;

5.

Rated for operation with a peak saturated power output greater than 1 W (30 dBm) at any frequency exceeding 37 GHz up to and including 43,5 GHz, and with a "fractional bandwidth" of greater than 10 %;

6.

Rated for operation with a peak saturated power output greater than 31,62 mW (15 dBm) at any frequency exceeding 43,5 GHz up to and including 75 GHz, and with a "fractional bandwidth" of greater than 10 %;

7.

Rated for operation with a peak saturated power output greater than 10 mW (10 dBm) at any frequency exceeding 75 GHz up to and including 90 GHz, and with a "fractional bandwidth" of greater than 5 %; or

8.

Rated for operation with a peak saturated power output greater than 0,1 nW (-70 dBm) at any frequency exceeding 90 GHz;

[5E101] "Technology" according to the General Technology Note for the "development", "production" or "use" of equipment specified in 5A101.

PART 2 — U.K. "INFORMATION SECURITY"
Note 1: The control status of "information security" items or functions is determined in Category 5, Part 2 even if they are components, "software" or functions of other systems or equipment.
Note 2: Category 5 – Part 2 does not control products when accompanying their user for the user's personal use.
Note 3: Cryptography Note 5A002 and 5D002 do not control items as follows:
a.

Items that meet all of the following:

1.

Generally available to the public by being sold, without restriction, from stock at retail selling points by means of any of the following:

a.

Over-the-counter transactions;

b.

Mail order transactions;

c.

Electronic transactions; or

d.

Telephone call transactions;

2.

The cryptographic functionality cannot easily be changed by the user;

3.

Designed for installation by the user without further substantial support by the supplier; and

4.

When necessary, details of the goods are accessible and will be provided, upon request, to the competent authorities of the Member State in which the exporter is established in order to ascertain compliance with conditions described in paragraphs 1. to 3. above;

b.

Hardware components or 'executable software', of existing items described in paragraph a. of this Note, that have been designed for these existing items, meeting all of the following:

1.

"Information security" is not the primary function or set of functions of the component or 'executable software';

2.

The component or 'executable software' does not change any cryptographic functionality of the existing items, or add new cryptographic functionality to the existing items;

3.

The feature set of the component or 'executable software' is fixed and is not designed or modified to customer specification; and

Note 4: Category 5 – Part 2 does not control items incorporating or using "cryptography" and meeting all of the following:
a.

The primary function or set of functions is not any of the following:

1.

"Information security";

2.

A computer, including operating systems, parts and components therefor;

3.

Sending, receiving or storing information (except in support of entertainment, mass commercial broadcasts, digital rights management or medical records management); or

4.

Networking (includes operation, administration, management and provisioning);

b.

The cryptographic functionality is limited to supporting their primary function or set of functions; and

c.

When necessary, details of the items are accessible and will be provided, upon request, to the competent authorities of the Member State in which the exporter is established in order to ascertain compliance with conditions described in paragraphs a. and b. above.

[5A2] Systems, Equipment and Components

[5A002] "Information security" systems, equipment and components therefor, as follows:

a.

Systems, equipment and components for "information security", as follows,

N.B.: For the control of Global Navigation Satellite Systems (GNSS) receiving equipment containing or employing decryption, see 7A005 and for related decryption "software" and "technology" see 7D005 and 7E001.
1.

Designed or modified to use "cryptography" employing digital techniques performing any cryptographic function other than authentication, digital signature or the execution of copy-protected "software", and having any of the following:

Technical Notes:
1. Functions for authentication, digital signature and the execution of copy-protected "software" include their associated key management function.
2. Authentication includes all aspects of access control where there is no encryption of files or text except as directly related to the protection of passwords, Personal Identification Numbers (PINs) or similar data to prevent unauthorised access.

Designed or modified to perform 'cryptanalytic functions';

Note: 5A002.a.2. includes systems or equipment, designed or modified to perform 'cryptanalytic functions' by means of reverse engineering.

Systems, equipment, and components, designed or modified to enable, by means of "cryptographic activation" an item to achieve or exceed the controlled performance levels for functionality specified by 5A002.a. that would not otherwise be enabled.

Note: 5A002 does not control any of the following:
a.

Smart cards and smart card 'readers/writers' as follows:

Cryptographic equipment specially designed and limited for banking use or 'money transactions';

Equipment, having no functionality specified by 5A002.a.2., 5A002.a.4., 5A002.a.7.,5A002.a.8 or 5A002.b. meeting all of the following:

[5B2] Test, Inspection and Production Equipment

[5B002] "Information security" test, inspection and "production" equipment, as follows:

a.

Equipment specially designed for the "development" or "production" of equipment specified in 5A002 or 5B002.b.;

b.

Measuring equipment specially designed to evaluate and validate the "information security" functions of the equipment specified in 5A002 or "software" specified in 5D002.a. or 5D002.c.

[5C2] Materials

None.

[5D2] Software

[5D002] "Software" as follows:

[5E2] Technology

[5E002] "Technology" as follows:

CATEGORY 6 — SENSORS AND LASERS
[6A] Systems, Equipment and Components

[6A001] [X1Acoustic systems, equipment and components, as follows:

a.

Marine acoustic systems, equipment and specially designed components therefor, as follows:

1.

Active (transmitting or transmitting-and-receiving) systems, equipment and specially designed components therefor, as follows:

Note: 6A001.a.1. does not control equipment as follows:
a.

Depth sounders operating vertically below the apparatus, not including a scanning function exceeding ± 20°, and limited to measuring the depth of water, the distance of submerged or buried objects or fish finding;

b.

Acoustic beacons, as follows:

1.

Acoustic emergency beacons;

2.

Pingers specially designed for relocating or returning to an underwater position.

a.

Acoustic seabed survey equipment as follows:

1.

Surface vessel survey equipment designed for seabed topographic mapping and having all of the following:

Underwater survey equipment designed for seabed topographic mapping and having any of the following:

Technical Note:

The acoustic sensor pressure rating determines the depth rating of the equipment specified in 6A001.a.1.a.2.

Acoustic projectors, including transducers, incorporating piezoelectric, magnetostrictive, electrostrictive, electrodynamic or hydraulic elements operating individually or in a designed combination and having any of the following:

Note 1: The control status of acoustic projectors, including transducers, specially designed for other equipment not specified in 6A001 is determined by the control status of the other equipment.
Note 2: 6A001.a.1.c. does not control electronic sources which direct the sound vertically only, or mechanical (e.g., air gun or vapour-shock gun) or chemical (e.g., explosive) sources.
Note 3: Piezoelectric elements specified in 6A001.a.1.c. include those made from lead-magnesium-niobate/lead-titanate (Pb(Mg 1/3 Nb 2/3 )O 3 -PbTiO 3 , or PMN-PT) single crystals grown from solid solution or lead-indium-niobate/lead-magnesium niobate/lead-titanate (Pb(In 1/2 Nb 1/2 )O 3 –Pb(Mg 1/3 Nb 2/3 )O 3 –PbTiO 3 , or PIN-PMN-PT) single crystals grown from solid solution.

Passive systems, equipment and specially designed components therefor, as follows:

Hydrophones having any of the following:

Note: The control status of hydrophones specially designed for other equipment is determined by the control status of the other equipment.
Technical Note:

Hydrophones consist of one or more sensing elements producing a single acoustic output channel. Those that contain multiple elements can be referred to as a hydrophone group.

1.

Incorporating continuous flexible sensing elements;

2.

Incorporating flexible assemblies of discrete sensing elements with either a diameter or length less than 20 mm and with a separation between elements of less than 20 mm;

3.

Having any of the following sensing elements:

a.

Optical fibres;

b.

'Piezoelectric polymer films' other than polyvinylidene-fluoride (PVDF) and its co-polymers {P(VDF-TrFE) and P(VDF-TFE)};

c.

'Flexible piezoelectric composites';

d.

Lead-magnesium-niobate/lead-titanate (i.e., Pb(Mg1/3Nb2/3)O3-PbTiO3, or PMN-PT) piezoelectric single crystals grown from solid solution; or

e.

Lead-indium-niobate/lead-magnesium niobate/lead-titanate (i.e., Pb(In1/2Nb1/2)O3–Pb(Mg1/3Nb2/3)O3–PbTiO3, or PIN-PMN-PT) piezoelectric single crystals grown from solid solution;

4.

A 'hydrophone sensitivity' better than – 180 dB at any depth with no acceleration compensation;

5.

Designed to operate at depths exceeding 35 m with acceleration compensation; or

6.

Designed for operation at depths exceeding 1 000 m;

Technical Notes:
1. 'Piezoelectric polymer film' sensing elements consist of polarised polymer film that is stretched over and attached to a supporting frame or spool (mandrel).
2. 'Flexible piezoelectric composite' sensing elements consist of piezoelectric ceramic particles or fibres combined with an electrically insulating, acoustically transparent rubber, polymer or epoxy compound, where the compound is an integral part of the sensing elements.

Towed acoustic hydrophone arrays having any of the following:

Technical Note:

Hydrophone arrays consist of a number of hydrophones providing multiple acoustic output channels.

[6A002] Optical sensors or equipment and components therefor, as follows:

N.B.: SEE ALSO 6A102.
a.

Optical detectors as follows:

1.

"Space-qualified" solid-state detectors as follows:

Image intensifier tubes and specially designed components therefor, as follows:

Note: 6A002.a.2. does not control non-imaging photomultiplier tubes having an electron sensing device in the vacuum space limited solely to any of the following:
a.

A single metal anode; or

b.

Metal anodes with a centre to centre spacing greater than 500 μm.

Technical Note:

'Charge multiplication' is a form of electronic image amplification and is defined as the generation of charge carriers as a result of an impact ionization gain process. 'Charge multiplication' sensors may take the form of an image intensifier tube, solid state detector or "focal plane array".

Non-"space-qualified" "focal plane arrays" as follows:

N.B.: 'Microbolometer' non-"space-qualified" "focal plane arrays" are only specified in 6A002.a.3.f.
Technical Note:

Linear or two-dimensional multi-element detector arrays are referred to as "focal plane arrays";

Note 1: 6A002.a.3. includes photoconductive arrays and photovoltaic arrays.
Note 2: 6A002.a.3. does not control:
Technical Note:

'Charge multiplication' is a form of electronic image amplification and is defined as the generation of charge carriers as a result of an impact ionization gain process. 'Charge multiplication' sensors may take the form of an image intensifier tube, solid state detector or "focal plane array".

a.

Non-"space-qualified" "focal plane arrays" having all of the following:

1.

Individual elements with a peak response within the wavelength range exceeding 900 nm but not exceeding 1 050 nm; and

2.

Any of the following:

a.

A response "time constant" of less than 0,5 ns; or

b.

Specially designed or modified to achieve 'charge multiplication' and having a maximum "radiant sensitivity" exceeding 10 mA/W;

b.

Non-"space-qualified" "focal plane arrays" having all of the following:

1.

Individual elements with a peak response in the wavelength range exceeding 1 050 nm but not exceeding 1 200 nm; and

2.

Any of the following:

a.

A response "time constant" of 95 ns or less; or

b.

Specially designed or modified to achieve 'charge multiplication' and having a maximum "radiant sensitivity" exceeding 10 mA/W;

c.

Non-"space-qualified" non-linear (2-dimensional) "focal plane arrays" having individual elements with a peak response in the wavelength range exceeding 1 200 nm but not exceeding 30 000 nm;

Non-"space-qualified" linear (1-dimensional) "focal plane arrays" having all of the following:

"Monospectral imaging sensors" and "multispectral imaging sensors", designed for remote sensing applications and having any of the following:

'Direct view' imaging equipment incorporating any of the following:

[6A003] Cameras, systems or equipment, and components therefor, as follows:

N.B.: SEE ALSO 6A203.
N.B.: For television and film-based photographic still cameras specially designed or modified for underwater use, see 8A002.d.1. and 8A002.e.
a.

Instrumentation cameras and specially designed components therefor, as follows:

Note: Instrumentation cameras, specified in 6A003.a.3. to 6A003.a.5., with modular structures should be evaluated by their maximum capability, using plug-ins available according to the camera manufacturer's specifications.

Imaging cameras as follows:

Note: 6A003.b. does not control television or video cameras, specially designed for television broadcasting.
1.

Video cameras incorporating solid state sensors, having a peak response in the wavelength range exceeding 10 nm, but not exceeding 30 000 nm and having all of the following:

a.

Having any of the following:

1.

More than 4 × 106 "active pixels" per solid state array for monochrome (black and white) cameras;

2.

More than 4 × 106 "active pixels" per solid state array for colour cameras incorporating three solid state arrays; or

3.

More than 12 × 106 "active pixels" for solid state array colour cameras incorporating one solid state array; and

b.

Having any of the following:

1.

Optical mirrors specified in 6A004.a.;

2.

Optical control equipment specified in 6A004.d.; or

3.

The capability for annotating internally generated 'camera tracking data';

Technical Note:
1. For the purpose of this entry, digital video cameras should be evaluated by the maximum number of "active pixels" used for capturing moving images.

Scanning cameras and scanning camera systems, having all of the following:

Imaging cameras incorporating "focal plane arrays" having any of the following:

Note 1: Imaging cameras specified in 6A003.b.4. include "focal plane arrays" combined with sufficient "signal processing" electronics, beyond the read out integrated circuit, to enable as a minimum the output of an analogue or digital signal once power is supplied.
Note 2: 6A003.b.4.a. does not control imaging cameras incorporating linear "focal plane arrays" with 12 elements or fewer, not employing time-delay-and-integration within the element and designed for any of the following:
a.

Industrial or civilian intrusion alarm, traffic or industrial movement control or counting systems;

b.

Industrial equipment used for inspection or monitoring of heat flows in buildings, equipment or industrial processes;

c.

Industrial equipment used for inspection, sorting or analysis of the properties of materials;

d.

Equipment specially designed for laboratory use; or

e.

Medical equipment.

Note 3: 6A003.b.4.b. does not control imaging cameras having any of the following:
a.

A maximum frame rate equal to or less than 9 Hz;

b.

Having all of the following:

1.

Having a minimum horizontal or vertical 'Instantaneous-Field-of-View (IFOV)' of at least 10 mrad/pixel (milliradians/pixel);

2.

Incorporating a fixed focal-length lens that is not designed to be removed;

3.

Not incorporating a 'direct view' display, and

4.

Having any of the following:

a.

No facility to obtain a viewable image of the detected field-of-view, or

b.

The camera is designed for a single kind of application and designed not to be user modified; or

c.

The camera is specially designed for installation into a civilian passenger land vehicle and having all of the following:

1.

The placement and configuration of the camera within the vehicle are solely to assist the driver in the safe operation of the vehicle;

2.

Is only operable when installed in any of the following:

a.

The civilian passenger land vehicle for which it was intended and the vehicle weighs less than 4,500 kg (gross vehicle weight); or

b.

A specially designed, authorized maintenance test facility; and

3.

Incorporates an active mechanism that forces the camera not to function when it is removed from the vehicle for which it was intended.

Technical Notes:
1. 'Instantaneous Field of View (IFOV)' specified in 6A003.b.4. Note 3.b. is the lesser figure of the 'Horizontal IFOV' or the 'Vertical IFOV'.

'Horizontal IFOV' = horizontal Field of View (FOV) / number of horizontal detector elements

'Vertical IFOV' = vertical Field of View (FOV) / number of vertical detector elements.

2. 'Direct view' in 6A003.b.4. Note 3.b. refers to an imaging camera operating in the infrared spectrum that presents a visual image to a human observer using a near-to-eye micro display incorporating any light-security mechanism.
Note 4: 6A003.b.4.c. does not control imaging cameras having any of the following:
a.

Having all of the following:

1.

Where the camera is specially designed for installation as an integrated component into indoor and wall-plug-operated systems or equipment, limited by design for a single kind of application, as follows;

a.

Industrial process monitoring, quality control, or analysis of the properties of materials;

b.

Laboratory equipment specially designed for scientific research;

c.

Medical equipment;

d.

Financial fraud detection equipment; and

2.

Is only operable when installed in any of the following:

a.

The system(s) or equipment for which it was intended; or

b.

A specially designed, authorised maintenance facility; and

3.

Incorporates an active mechanism that forces the camera not to function when it is removed from the system(s) or equipment for which it was intended;

b.

Where the camera is specially designed for installation into a civilian passenger land vehicle or passenger and vehicle ferries, and having all of the following:

1.

The placement and configuration of the camera within the vehicle or ferry is solely to assist the driver or operator in the safe operation of the vehicle or ferry;

2.

Is only operable when installed in any of the following:

a.

The civilian passenger land vehicle for which it was intended; and the vehicle weighs less than 4,500 kg (gross vehicle weight);

b.

The passenger and vehicle ferry for which it was intended and having a length overall (LOA) 65 m or greater; or

c.

A specially designed, authorised maintenance test facility; and

3.

Incorporates an active mechanism that forces the camera not to function when it is removed from the vehicle for which it was intended;

c.

Limited by design to have a maximum "radiant sensitivity" of 10 mA/W or less for wavelengths exceeding 760 nm, having all of the following:

1.

Incorporating a response limiting mechanism designed not to be removed or modified;

2.

Incorporates an active mechanism that forces the camera not to function when the response limiting mechanism is removed; and

3.

Not specially designed or modified for underwater use: or

d.

Having all of the following:

1.

Not incorporating a 'direct view' or electronic image display;

2.

Has no facility to output a viewable image of the detected field of view;

3.

The "focal plane array" is only operable when installed in the camera for which it was intended; and

4.

The "focal plane array" incorporates an active mechanism that forces it to be permanently inoperable when removed from the camera for which it was intended

[6A004] Optical equipment and components, as follows:

a.

Optical mirrors (reflectors) as follows:

Technical Note:

For the purpose of 6A004.a., Laser Induced Damage Threshold (LIDT) is measured according to ISO 21254-1:2011.

Technical Notes:
1. An 'aspheric optical element' is any element used in an optical system whose imaging surface or surfaces are designed to depart from the shape of an ideal sphere.
2. Manufacturers are not required to measure the surface roughness listed in 6A004.e.2. unless the optical element was designed or manufactured with the intent to meet, or exceed, the control parameter.
Note 6A004.e. does not control 'aspheric optical elements' having any of the following:
a.

Largest optical-aperture dimension less than 1 m and focal length to aperture ratio equal to or greater than 4,5:1;

b.

Largest optical-aperture dimension equal to or greater than 1 m and focal length to aperture ratio equal to or greater than 7:1;

c.

Designed as Fresnel, flyeye, stripe, prism or diffractive optical elements;

d.

Fabricated from borosilicate glass having a coefficient of linear thermal expansion greater than 2,5 × 10–6 /K at 25 °C; or

e.

An x-ray optical element having inner mirror capabilities (e.g., tube-type mirrors).

N.B. For 'aspheric optical elements' specially designed for lithography equipment, see 3B001.

[6A005] "Lasers", other than those specified in 0B001.g.5. or 0B001.h.6., components and optical equipment, as follows:

N.B.: SEE ALSO 6A205.
Note 1: Pulsed "lasers" include those that run in a continuous wave (CW) mode with pulses superimposed.
Note 2: Excimer, semiconductor, chemical, CO, CO2, and 'non-repetitive pulsed' Nd:glass "lasers" are only specified in 6A005.d.
Technical Note:

'Non-repetitive pulsed' refers to "lasers" that produce either a single output pulse or that have a time interval between pulses exceeding one minute.

Note 3: 6A005 includes fibre "lasers".
Note 4: The control status of "lasers" incorporating frequency conversion (i.e., wavelength change) by means other than one "laser" pumping another "laser" is determined by applying the control parameters for both the output of the source "laser" and the frequency-converted optical output.
Note 5: 6A005 does not control "lasers" as follows:
a.

Ruby with output energy below 20 J;

b.

Nitrogen;

c.

Krypton.

Technical Note:

In 6A005 'Wall-plug efficiency' is defined as the ratio of "laser" output power (or "average output power") to total electrical input power required to operate the "laser", including the power supply/conditioning and thermal conditioning/heat exchanger.

a.

Non-"tunable" continuous wave "(CW) lasers" having any of the following:

1.

Output wavelength less than 150 nm and output power exceeding 1 W;

2.

Output wavelength of 150 nm or more but not exceeding 510 nm and output power exceeding 30 W;

Output wavelength exceeding 975 nm but not exceeding 1 150 nm and any of the following:

Note 1: 6A005.a.6.b. does not control multiple transverse mode, industrial "lasers" with output power exceeding 2 kW and not exceeding 6 kW with a total mass greater than 1 200 kg. For the purpose of this note, total mass includes all components required to operate the "laser", e.g., "laser", power supply, heat exchanger, but excludes external optics for beam conditioning and/or delivery.
Note 2: 6A005.a.6.b. does not control multiple transverse mode, industrial "lasers" having any of the following:
a.

Output power exceeding 500 W but not exceeding 1 kW and having all of the following:

1.

Beam Parameter Product (BPP) exceeding 0,7 mm•mrad; and

2.

'Brightness' not exceeding 1024 W/(mm•mrad)2;

b.

Output power exceeding 1 kW but not exceeding 1.6 kW and having a BPP exceeding 1,25 mm•mrad

c.

Output power exceeding 1,6 kW but not exceeding 2,5 kW and having a BPP exceeding 1,7 mm•mrad;

d.

Output power exceeding 2,5 kW but not exceeding 3,3 kW and having a BPP exceeding 2,5 mm•mrad;

e.

Output power exceeding 3,3 kW but not exceeding 4 kW and having a BPP exceeding 3,5 mm•mrad;

f.

Output power exceeding 4 kW but not exceeding 5 kW and having a BPP exceeding 5 mm•mrad;

g.

Output power exceeding 5 kW but not exceeding 6 kW and having a BPP exceeding 7,2 mm•mrad;

h.

Output power exceeding 6 kW but not exceeding 8 kW and having a BPP exceeding 12 mm•mrad; or

i.

Output power exceeding 8 kW but not exceeding 10 kW and having a BPP exceeding 24 mm•mrad.

Non-"tunable" "pulsed lasers" having any of the following:

Output wavelength of 150 nm or more but not exceeding 510 nm and any of the following:

Output wavelength exceeding 975 nm but not exceeding 1,150 nm and any of the following:

"Tunable" "lasers" having any of the following:

Other "lasers", not specified in 6A005.a., 6A005.b. or 6A005.c. as follows:

Semiconductor "lasers" as follows:

Note 1: 6A005.d.1. includes semiconductor "lasers" having optical output connectors (e.g., fibre optic pigtails).
Note 2: The control status of semiconductor "lasers" specially designed for other equipment is determined by the control status of the other equipment.
a.

Individual single-transverse mode semiconductor "lasers" having any of the following:

1.

Wavelength equal to or less than 1 510 nm and average or CW output power, exceeding 1,5 W; or

2.

Wavelength greater than 1 510 nm and average or CW output power, exceeding 500 mW;

b.

Individual, multiple-transverse mode semiconductor "lasers" having any of the following:

1.

Wavelength of less than 1 400 nm and average or CW output power, exceeding 15 W;

2.

Wavelength equal to or greater than 1 400 nm and less than 1 900 nm and average or CW output power, exceeding 2,5 W; or

3.

Wavelength equal to or greater than 1 900 nm and average or CW output power, exceeding 1 W;

c.

Individual semiconductor "laser" 'bars', having any of the following:

1.

Wavelength of less than 1 400 nm and average or CW output power, exceeding 100 W;

2.

Wavelength equal to or greater than 1 400 nm and less than 1 900 nm and average or CW output power, exceeding 25 W; or

3.

Wavelength equal to or greater than 1 900 nm and average or CW output power, exceeding 10 W;

d.

Semiconductor "laser" 'stacked arrays' (two-dimensional arrays) having any of the following:

1.

Wavelength less than 1 400 nm and having any of the following:

a.

Average or CW total output power less than 3 kW and having average or CW output 'power density' greater than 500 W/cm2;

b.

Average or CW total output power equal to or exceeding 3 kW but less than or equal to 5 kW, and having average or CW output 'power density' greater than 350 W/cm2;

c.

Average or CW total output power exceeding 5 kW;

d.

Peak pulsed 'power density' exceeding 2 500 W/cm2; or

e.

Spatially coherent average or CW total output power, greater than 150 W;

2.

Wavelength greater than or equal to 1 400 nm but less than 1 900 nm, and having any of the following:

a.

Average or CW total output power less than 250 W and average or CW output 'power density' greater than 150 W/cm2;

b.

Average or CW total output power equal to or exceeding 250 W but less than or equal to 500 W, and having average or CW output 'power density' greater than 50 W/cm2;

c.

Average or CW total output power exceeding 500 W;

d.

Peak pulsed 'power density' exceeding 500 W/cm2; or

e.

Spatially coherent average or CW total output power, exceeding 15 W

3.

Wavelength greater than or equal to 1 900 nm and having any of the following:

a.

Average or CW output 'power density' greater than 50 W/cm2;

b.

Average or CW output power greater than 10 W; or

c.

Spatially coherent average or CW total output power, exceeding 1,5 W; or

4.

At least one "laser" 'bar' specified in 6A005.d.1.c.;

Semiconductor "laser" 'stacked arrays', other than those specified in 6A005.d.1.d., having all of the following:

Components as follows:

Mirrors cooled either by 'active cooling' or by heat pipe cooling;

[6A006] "Magnetometers", "magnetic gradiometers", "intrinsic magnetic gradiometers", underwater electric field sensors, "compensation systems", and specially designed components therefor, as follows:

N.B.: SEE ALSO 7A103.d.
Note: 6A006 does not control instruments specially designed for fishery applications or biomagnetic measurements for medical diagnostics.
a.

"Magnetometers" and subsystems as follows:

1.

"Magnetometers" using "superconductive" (SQUID) "technology" and having any of the following:

a.

SQUID systems designed for stationary operation, without specially designed subsystems designed to reduce in-motion noise, and having a 'sensitivity' equal to or lower (better) than 50 fT (rms) per square root Hz at a frequency of 1 Hz; or

b.

SQUID systems having an in-motion-magnetometer 'sensitivity' lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz and specially designed to reduce in-motion noise;

2.

"Magnetometers" using optically pumped or nuclear precession (proton/Overhauser) "technology" having a 'sensitivity' lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz;

3.

"Magnetometers" using fluxgate "technology" having a 'sensitivity' equal to or lower (better) than 10 pT (rms) per square root Hz at a frequency of 1 Hz;

4.

Induction coil "magnetometers" having a 'sensitivity' lower (better) than any of the following:

a.

0,05 nT (rms) per square root Hz at frequencies of less than 1 Hz;

b.

1 × 10–3 nT (rms) per square root Hz at frequencies of 1 Hz or more but not exceeding 10 Hz; or

c.

1 × 10–4 nT (rms) per square root Hz at frequencies exceeding 10 Hz;

5.

Fibre optic "magnetometers" having a 'sensitivity' lower (better) than 1 nT (rms) per square root Hz;

b.

Underwater electric field sensors having a 'sensitivity' lower (better) than 8 nanovolt per metre per square root Hz when measured at 1 Hz;

c.

"Magnetic gradiometers" as follows:

1.

"Magnetic gradiometers" using multiple "magnetometers" specified in 6A006.a.;

2.

Fibre optic "intrinsic magnetic gradiometers" having a magnetic gradient field 'sensitivity' lower (better) than 0,3 nT/m rms per square root Hz;

3.

"Intrinsic magnetic gradiometers", using "technology" other than fibre-optic "technology", having a magnetic gradient field 'sensitivity' lower (better) than 0,015 nT/m rms per square root Hz;

d.

"Compensation systems" for magnetic or underwater electric field sensors resulting in a performance equal to or better than the specified parameters of 6A006.a., 6A006.b. or 6A006.c.;

e.

Underwater electromagnetic receivers incorporating magnetic field sensors specified by 6A006.a. or underwater electric field sensors specified by 6A006.b.

Technical Note:

For the purposes of 6A006., 'sensitivity' (noise level) is the root mean square of the device-limited noise floor which is the lowest signal that can be measured.

[6A007] Gravity meters (gravimeters) and gravity gradiometers, as follows:

N.B.: SEE ALSO 6A107.

[6A008] Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor:

N.B.: SEE ALSO 6A108.
Note: 6A008 does not control:
  • Secondary surveillance radar (SSR);

  • Civil Automotive Radar;

  • Displays or monitors used for air traffic control (ATC);

  • Meteorological (weather) radar;

  • Precision approach radar (PAR) equipment conforming to ICAO standards and employing electronically steerable linear (1-dimensional) arrays or mechanically positioned passive antennae.

a.

Operating at frequencies from 40 GHz to 230 GHz and having any of the following:

1.

An average output power exceeding 100 mW; or

2.

Locating accuracy of 1 m or less (better) in range and 0,2 degree or less (better) in azimuth;

b.

A tunable bandwidth exceeding ± 6,25 % of the 'centre operating frequency';

Providing ground-based operation with a maximum "instrumented range" exceeding 185 km;

Being "laser" radar or Light Detection and Ranging (LIDAR) equipment and having any of the following:

Note 1: LIDAR equipment specially designed for surveying is only specified in 6A008.j.3.
Note 2: 6A008.j. does not control LIDAR equipment specially designed for meteorological observation.
Note 3: Parameters in the IHO Order 1a Standard 5th Edition February 2008 are summarized as follows:
k.

Having "signal processing" sub-systems using "pulse compression" and having any of the following:

Having data processing sub-systems and having any of the following:

Technical Notes:
1. For the purposes of 6A008, 'marine radar' is a radar that is used to navigate safely at sea, inland waterways or near-shore environments.
2. For the purposes of 6A008, 'vessel traffic service' is a vessel traffic monitoring and control service similar to air traffic control for aircraft.

[6A102] Radiation hardened 'detectors', other than those specified in 6A002, specially designed or modified for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects) and usable for "missiles", designed or rated to withstand radiation levels which meet or exceed a total irradiation dose of 5 × 105 rads (silicon).

Technical Note:

In 6A102, a 'detector' is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure.

[6A107] Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows:

a.

Gravity meters, other than those specified in 6A007.b, designed or modified for airborne or marine use, and having a static or operational accuracy equal to or less (better) than 0,7 milligal (mgal), and having a time-to-steady-state registration of two minutes or less;

b.

Specially designed components for gravity meters specified in 6A007.b or 6A107.a. and gravity gradiometers specified in 6A007.c.

[6A108] Radar systems and tracking systems, other than those specified in entry 6A008, as follows:

Technical Note:

In 6A108.b. 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[6A202] Photomultiplier tubes having both of the following characteristics:

a.

Photocathode area of greater than 20 cm2; and

b.

Anode pulse rise time of less than 1 ns.

[6A203] Cameras and components, other than those specified in 6A003, as follows:

N.B. 1: "Software" specially designed to enhance or release the performance of a camera or imaging device to meet the characteristics of 6A203.a., 6A203.b. or 6A203.c. is specified in 6D203.
N.B. 2: "Technology" in the form of codes or keys to enhance or release the performance of a camera or imaging device to meet the characteristics of 6A203.a., 6A203.b. or 6A203.c is specified in 6E203.
Note: 6A203.a. to 6A203.c. does not control cameras or imaging devices if they have hardware, "software" or "technology" constraints that limit the performance to less than that specified above, provided they meet any of the following:
1.

They need to be returned to the original manufacturer to make the enhancements or release the constraints;

2.

They require "software" as specified in 6D203 to enhance or release the performance to meet the characteristics of 6A203; or

3.

They require "technology" in the form of keys or codes as specified in 6E203 to enhance or release the performance to meet the characteristics of 6A203.

a.

Streak cameras, and specially designed components therefor, as follows:

1.

Streak cameras with writing speeds greater than 0,5 mm/μs;

2.

Electronic streak cameras capable of 50 ns or less time resolution;

3.

Streak tubes for cameras specified in 6A203.a.2.;

4.

Plug-ins specially designed for use with streak cameras which have modular structures and that enable the performance specifications in 6A203.a.1. or 6A203.a.2.;

5.

Synchronizing electronics units, rotor assemblies consisting of turbines, mirrors and bearings specially designed for cameras specified in 6A203.a.1.;

b.

Framing cameras, and specially designed components therefor, as follows:

[6A205] "Lasers", "laser" amplifiers and oscillators, other than those specified in 0B001.g.5., 0B001.h.6. and 6A005; as follows:

N.B.: For copper vapour lasers, see 6A005.b.
a.

Argon ion "lasers" having both of the following characteristics:

1.

Operating at wavelengths between 400 nm and 515 nm; and

2.

An average output power greater than 40 W;

b.

Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:

1.

Operating at wavelengths between 300 nm and 800 nm;

2.

An average output power greater than 1 W;

3.

A repetition rate greater than 1 kHz; and

4.

Pulse width less than 100 ns;

c.

Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:

1.

Operating at wavelengths between 300 nm and 800 nm;

2.

An average output power greater than 30 W;

3.

A repetition rate greater than 1 kHz; and

4.

Pulse width less than 100 ns;

[6A225] Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.

Note: 6A225 includes velocity interferometers such as VISARs (Velocity Interferometer Systems for Any Reflector), DLIs (Doppler Laser Interferometers) and PDV (Photonic Doppler Velocimeters) also known as Het-V (Heterodyne Velocimeters).

[6A226] Pressure sensors, as follows:

a.

Shock pressure gauges capable of measuring pressures greater than 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene bifluoride (PVBF, PVF2);

b.

Quartz pressure transducers for pressures greater than 10 GPa.

[6B] Test, Inspection and Production Equipment

[6B004] Optical equipment as follows:

[6B007] Equipment to produce, align and calibrate land-based gravity meters with a static accuracy of better than 0.1 mGal.

[6B008] Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor.

N.B.: SEE ALSO 6B108.

[6B108] Systems, other than those specified in 6B008, specially designed for radar cross section measurement usable for 'missiles' and their subsystems.

Technical Note:

In 6B108 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[6C] Materials

[6C002] Optical sensor materials as follows:

[6C004] Optical materials as follows:

a.

Zinc selenide (ZnSe) and zinc sulphide (ZnS) "substrate blanks", produced by the chemical vapour deposition process and having any of the following:

1.

A volume greater than 100 cm3; or

2.

A diameter greater than 80 mm and a thickness of 20 mm or more;

b.

Electro-optic materials and non-linear optical materials, as follows:

1.

Potassium titanyl arsenate (KTA) (CAS 59400-80-5);

2.

Silver gallium selenide (AgGaSe2, also known as AGSE) (CAS 12002-67-4);

3.

Thallium arsenic selenide (Tl3AsSe3, also known as TAS) (CAS 16142-89-5);

4.

Zinc germanium phosphide (ZnGeP2, also known as ZGP, zinc germanium biphosphide or zinc germanium diphosphide); or

5.

Gallium selenide (GaSe) (CAS 12024-11-2);

c.

Non-linear optical materials, other than those specified in 6C004.b., having any of the following:

1.

Having all of the following:

a.

Dynamic (also known as non-stationary) third order non-linear susceptibility (χ(3), chi 3) of 10–6 m2/V2 or more; and

b.

Response time of less than 1 ms; or

2.

Second order non-linear susceptibility (χ(2), chi 2) of 3,3 × 10–11 m/V or more;

d.

"Substrate blanks" of silicon carbide or beryllium beryllium (Be/Be) deposited materials, exceeding 300 mm in diameter or major axis length;

e.

Glass, including fused silica, phosphate glass, fluorophosphate glass, zirconium fluoride (ZrF4) (CAS 7783-64-4) and hafnium fluoride (HfF4) (CAS 13709-52-9) and having all of the following:

1.

A hydroxyl ion (OH-) concentration of less than 5 ppm;

2.

Integrated metallic purity levels of less than 1 ppm; and

3.

High homogeneity (index of refraction variance) less than 5 × 10–6;

f.

Synthetically produced diamond material with an absorption of less than 10–5 cm–1 for wavelengths exceeding 200 nm but not exceeding 14,000 nm.

[6C005] "Laser" materials as follows:

a.

Synthetic crystalline "laser" host material in unfinished form as follows:

1.

Titanium doped sapphire;

2.

Not used.

b.

Rare-earth-metal doped double-clad fibres having any of the following:

[6D] Software

[6D001] "Software" specially designed for the "development" or "production" of equipment specified in 6A004, 6A005, 6A008 or 6B008.

[6D002] "Software" specially designed for the "use" of equipment specified in 6A002.b., 6A008 or 6B008.

[6D003] Other "software" as follows:

a.

"Software" as follows:

[6D102] "Software" specially designed or modified for the "use" of goods specified in 6A108.

[6D103] "Software" which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for 'missiles'.

Technical Note:

In 6D103 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[6D203] "Software" specially designed to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203.a. to 6A203.c.

[6E] Technology

[6E001] "Technology" according to the General Technology Note for the "development" of equipment, materials or "software" specified in 6A, 6B, 6C or 6D.

[6E002] "Technology" according to the General Technology Note for the "production" of equipment or materials specified in 6A, 6B or 6C.

[6E003] Other "technology" as follows:

[6E101] "Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 6A002, 6A007.b. and c., 6A008, 6A102, 6A107, 6A108, 6B108, 6D102 or 6D103.

Note: 6E101 only specifies "technology" for equipment specified in 6A008 When it is designed for airborne applications and is usable in "missiles".

[6E201] "Technology" according to the General Technology Note for the "use" of equipment specified in 6A003, 6A005.a.2., 6A005.b.2., 6A005.b.3., 6A005.b.4., 6A005.b.6., 6A005.c.2., 6A005.d.3.c., 6A005.d.4.c., 6A202, 6A203, 6A205, 6A225 or 6A226.

[6E203] "Technology", in the form of codes or keys, to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203a. to 6A203.c.

CATEGORY 7 — NAVIGATION AND AVIONICS
[7A] Systems, Equipment and Components
N.B.: For automatic pilots for underwater vehicles, see Category 8. For radar, see Category 6.

[7A001] Accelerometers as follows and specially designed components therefor:

N.B.: SEE ALSO 7A101.
N.B.: For angular or rotational accelerometers, see 7A001.b.

[7A002] Gyros or angular rate sensors, having any of the following and specially designed components therefor:

N.B.: SEE ALSO 7A102.
N.B.: For angular or rotational accelerometers, see 7A001.b.

[7A003] 'Inertial measurement equipment or systems', having any of the following:

N.B.: SEE ALSO 7A103.
Note 1: 'Inertial measurement equipment or systems' incorporate accelerometers or gyroscopes to measure changes in velocity and orientation in order to determine or maintain heading or position without requiring an external reference once aligned. 'Inertial measurement equipment or systems' include:
  • Attitude and Heading Reference Systems (AHRSs);

  • Gyrocompasses;

  • Inertial Measurement Units (IMUs);

  • Inertial Navigation Systems (INSs);

  • Inertial Reference Systems (IRSs);

  • Inertial Reference Units (IRUs).

Note 2: 7A003 does not control 'inertial measurement equipment or systems' which are certified for use on "civil aircraft" by civil aviation authorities of one or more EU Member States or Wassenaar Arrangement Participating States.
Technical Notes:
1. 'Positional aiding references' independently provide position, and include:
a.

Global Navigation Satellite Systems (GNSS);

b.

"Data-Based Referenced Navigation" ("DBRN").

2. 'Circular Error Probable' ('CEP') - In a circular normal distribution, the radius of the circle containing 50 % of the individual measurements being made, or the radius of the circle within which there is a 50 % probability of being located.
a.

Designed for "aircraft", land vehicles or vessels, providing position without the use of 'positional aiding references', and having any of the following accuracies subsequent to normal alignment:

Designed for "aircraft", land vehicles or vessels, with an embedded 'positional aiding reference' and providing position after loss of all 'positional aiding references' for a period of up to 4 minutes, having an accuracy of less (better) than 10 meters 'CEP';

[7A004] 'Star trackers' and components therefor, as follows:

N.B.: SEE ALSO 7A104.
a.'Star trackers' with a specified azimuth accuracy of equal to or less (better) than 20 seconds of arc throughout the specified lifetime of the equipment;
b.Components specially designed for equipment specified in 7A004.a. as follows:
1.

Optical heads or baffles;

2.

Data processing units.

Technical Note:

'Star trackers' are also referred to as stellar attitude sensors or gyro-astro compasses.

[7A005] Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following and specially designed components therefor:

N.B.: SEE ALSO 7A105.
N.B.: For equipment specially designed for military use, see Military Goods Controls.
a.

Employing a decryption algorithm specially designed or modified for government use to access the ranging code for position and time; or

[7A006] Airborne altimeters operating at frequencies other than 4.2 to 4.4 GHz inclusive and having any of the following:

N.B.: SEE ALSO 7A106.
a.

"Power management"; or

b.

Using phase shift key modulation.

[7A008] Underwater sonar navigation systems using doppler velocity or correlation velocity logs integrated with a heading source and having a positioning accuracy of equal to or less (better) than 3 % of distance travelled 'Circular Error Probable' ('CEP') and specially designed components therefor.

Note: 7A008 does not control systems specially designed for installation on surface vessels or systems requiring acoustic beacons or buoys to provide positioning data.
N.B.: See 6A001.a. for acoustic systems, and 6A001.b. for correlation-velocity and Doppler-velocity sonar log equipment.

See 8A002 for other marine systems.

[7A101] Linear accelerometers, other than those specified in 7A001, designed for use in inertial navigation systems or in guidance systems of all types, usable in 'missiles', having all the following characteristics, and specially designed components therefor:

a.

A "bias" "repeatability" of less (better) than 1 250 micro g; and

b.

A "scale factor" "repeatability" of less (better) than 1 250 ppm;

Note: 7A101 does not control accelerometers specially designed and developed as Measurement While Drilling (MWD) Sensors for use in downhole well service operations.
Technical Notes:
1. In 7A101 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km;
2. In 7A101 the measurement of "bias" and "scale factor" refers to a one sigma standard deviation with respect to a fixed calibration over a period of one year;

[7A102] All types of gyros, other than those specified in 7A002, usable in 'missiles', with a rated "drift rate" 'stability' of less than 0.5 ° (1 sigma or rms) per hour in a 1 g environment and specially designed components therefor.

Technical Notes:
1. In 7A102 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
2. In 7A102 'stability' is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition (IEEE STD 528-2001 paragraph 2,247).

[7A103] Instrumentation, navigation equipment and systems, other than those specified in 7A003, as follows; and specially designed components therefor:

a.

Inertial or other equipment, using accelerometers or gyros as follows, and systems incorporating such equipment:

1.

Accelerometers specified in 7A001.a.3., 7A001.b. or 7A101 or gyros specified in 7A002 or 7A102; or

2.

Accelerometers specified in 7A001,a,1, or 7A001,a,2, designed for use in inertial navigation systems or in guidance systems of all types, and usable in 'missiles';

'Integrated navigation systems', designed or modified for 'missiles' and capable of providing a navigational accuracy of 200 m Circle of Equal Probability (CEP) or less;

[7A104] Gyro-astro compasses and other devices, other than those specified in 7A004, which derive position or orientation by means of automatically tracking celestial bodies or satellites and specially designed components therefor.

[7A105] Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS, or Galileo), other than those specified in 7A005, having any of the following characteristics, and specially designed components therefor:

[7A106] Altimeters, other than those specified in 7A006, of radar or laser radar type, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

[7A115] Passive sensors for determining bearing to specific electromagnetic source (direction finding equipment) or terrain characteristics, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

Note: 7A115 includes sensors for the following equipment:
a.

Terrain contour mapping equipment;

b.

Imaging sensor equipment (both active and passive);

c.

Passive interferometer equipment.

[7A116] Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

a.

Hydraulic, mechanical, electro-optical, or electro-mechanical flight control systems (including fly-by-wire types);

b.

Attitude control equipment;

c.

Flight control servo valves designed or modified for the systems specified in 7A116.a. or 7A116.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.

[7A117] "Guidance sets", usable in "missiles" capable of achieving system accuracy of 3,33 % or less of the range (e.g., a "CEP" of 10 km or less at a range of 300 km).

[7B] Test, Inspection and Production Equipment

[7B001] Test, calibration or alignment equipment, specially designed for equipment specified in 7A.

Note: 7B001 does not control test, calibration or alignment equipment for 'Maintenance Level I' or 'Maintenance Level II'.
Technical Notes:
1. 'Maintenance Level I'

The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare.

2. 'Maintenance Level II'

The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. 'Maintenance Level II' does not include the disassembly or repair of controlled accelerometers or gyro sensors.

[7B002] Equipment specially designed to characterize mirrors for ring "laser" gyros, as follows:

N.B.: SEE ALSO 7B102.
a.

Scatterometers having a measurement accuracy of 10 ppm or less (better);

b.

Profilometers having a measurement accuracy of 0,5 nm (5 angstrom) or less (better).

[7B003] Equipment specially designed for the "production" of equipment specified in 7A.

Note: 7B003 includes:
  • Gyro tuning test stations;

  • Gyro dynamic balance stations;

  • Gyro run-in/motor test stations;

  • Gyro evacuation and fill stations;

  • Centrifuge fixtures for gyro bearings;

  • Accelerometer axis align stations;

  • Fibre optic gyro coil winding machines.

[7B102] Reflectometers specially designed to characterise mirrors, for "laser" gyros, having a measurement accuracy of 50 ppm or less (better).

[7B103] "Production facilities" and "production equipment" as follows:

a.

"Production facilities" specially designed for equipment specified in 7A117;

b.

"Production equipment", and other test, calibration and alignment equipment, other than that specified in 7B001 to 7B003, designed or modified to be used with equipment specified in 7A.

[7C] Materials

None.

[7D] Software

[7D001] "Software" specially designed or modified for the "development" or "production" of equipment specified in 7A. or 7B.

[7D002] "Source code" for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems ('AHRS').

Note: 7D002 does not control "source code" for the "use" of gimballed 'AHRS'.
Technical Note:

'AHRS' generally differ from Inertial Navigation Systems (INS) in that an 'AHRS' provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.

[7D003] Other "software" as follows:

a.

"Software" specially designed or modified to improve the operational performance or reduce the navigational error of systems to the levels specified in 7A003, 7A004 or 7A008;

b.

"Source code" for hybrid integrated systems which improves the operational performance or reduces the navigational error of systems to the level specified in 7A003 or 7A008 by continuously combining heading data with any of the following:

1.

Doppler radar or sonar velocity data;

2.

Global Navigation Satellite Systems (GNSS) reference data; or

3.

Data from "Data-Based Referenced Navigation" ("DBRN") systems;

c.

Not used;

d.

Not used;

e.

Computer-Aided-Design (CAD) "software" specially designed for the "development" of "active flight control systems", helicopter multi-axis fly-by-wire or fly-by-light controllers or helicopter "circulation controlled anti-torque or circulation-controlled direction control systems", whose "technology" is specified in 7E004.b., 7E004.c.1. or 7E004.c.2.

[7D004] "Source code" incorporating "development" "technology" specified in 7E004.a.1. to 7E004.a.6. or 7E004.b.,for any of the following:

a.

Digital flight management systems for "total control of flight";

b.

Integrated propulsion and flight control systems;

c.

"Fly-by-wire systems" or "fly-by-light systems";

d.

Fault-tolerant or self-reconfiguring "active flight control systems";

e.

Not used;

f.

Air data systems based on surface static data; or

g.

Three dimensional displays.

Note: 7D004. does not control "source code" associated with common computer elements and utilities (e.g., input signal acquisition, output signal transmission, computer program and data loading, built-in test, task scheduling mechanisms) not providing a specific flight control system function.

[7D005] "Software" specially designed to decrypt Global Navigation Satellite Systems (GNSS) ranging code designed for government use.

[7D101] "Software" specially designed or modified for the "use" of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.

[7D102] Integration "software" as follows:

[7D103] "Software" specially designed for modelling or simulation of the "guidance sets" specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

Note: "Software" specified in 7D103 remains controlled when combined with specially designed hardware specified in 4A102.
[7E] Technology

[7E001] "Technology" according to the General Technology Note for the "development" of equipment or "software", specified in 7A, 7B, 7D001, 7D002, 7D003, 7D005 and 7D101 to 7D103.

Note: 7E001 includes key management "technology" exclusively for equipment specified in 7A005.a.

[7E002] "Technology" according to the General Technology Note for the "production" of equipment specified in 7A or 7B.

[7E003] "Technology" according to the General Technology Note for the repair, refurbishing or overhaul of equipment specified in 7A001 to 7A004.

Note: 7E003 does not control maintenance "technology" directly associated with calibration, removal or replacement of damaged or unserviceable LRUs and SRAs of a "civil aircraft" as described in 'Maintenance Level I' or 'Maintenance Level II'.
N.B.: See Technical Notes to 7B001.

[7E004] Other "technology" as follows:

a.

"Technology" for the "development" or "production" of any of the following:

1.

Not used;

2.

Air data systems based on surface static data only, i.e., which dispense with conventional air data probes;

3.

Three dimensional displays for "aircraft";

4.

Not used;

5.

Electric actuators (i.e., electromechanical, electrohydrostatic and integrated actuator package) specially designed for "primary flight control";

6.

"Flight control optical sensor array" specially designed for implementing "active flight control systems"; or

7.

"DBRN" systems designed to navigate underwater, using sonar or gravity databases, that provide a positioning accuracy equal to or less (better) than 0.4 nautical miles;

b.

"Development" "technology", as follows, for "active flight control systems" (including "fly-by-wire systems" or "fly-by-light systems"):

1.

Photonic-based "technology" for sensing aircraft or flight control component state, transferring flight control data, or commanding actuator movement, "required" for "fly-by-light systems" "active flight control systems";

2.

Not used;

3.

Real-time algorithms to analyze component sensor information to predict and preemptively mitigate impending degradation and failures of components within an "active flight control system";

Real-time algorithms to identify component failures and reconfigure force and moment controls to mitigate "active flight control system" degradations and failures;

Integration of digital flight control, navigation and propulsion control data, into a digital flight management system for "total control of flight";

"Technology" "required" for deriving the functional requirements for "fly-by-wire systems" having all of the following:

[7E101] "Technology" according to the General Technology Note for the "use" of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115 to 7A117, 7B001, 7B002, 7B003, 7B102, 7B103, 7D101 to 7D103.

[7E102] "Technology" for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from external sources, as follows:

a.

Design "technology" for shielding systems;

b.

Design "technology" for the configuration of hardened electrical circuits and subsystems;

c.

Design "technology" for the determination of hardening criteria of 7E102.a. and 7E102.b.

[7E104] "Technology" for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory.

CATEGORY 8 — MARINE
[8A] Systems, Equipment and Components

[8A001] Submersible vehicles and surface vessels, as follows:

Note: For the control status of equipment for submersible vehicles, see:
  • Category 5, Part 2 "Information Security" for encrypted communication equipment;

  • Category 6 for sensors;

  • Categories 7 and 8 for navigation equipment;

  • Category 8A for underwater equipment.

a.

Manned, tethered submersible vehicles designed to operate at depths exceeding 1 000 m;

b.

Manned, untethered submersible vehicles having any of the following:

1.

Designed to 'operate autonomously' and having a lifting capacity of all the following:

a.

10 % or more of their weight in air; and

b.

15 kN or more;

2.

Designed to operate at depths exceeding 1 000 m; or

3.

Having all of the following:

a.

Designed to continuously 'operate autonomously' for 10 hours or more; and

b.

'Range' of 25 nautical miles or more;

Technical Notes:
1. For the purposes of 8A001.b., 'operate autonomously' means fully submerged, without snorkel, all systems working and cruising at minimum speed at which the submersible can safely control its depth dynamically by using its depth planes only, with no need for a support vessel or support base on the surface, sea-bed or shore, and containing a propulsion system for submerged or surface use.

[8A002] Marine systems, equipment and components, as follows:

Note: For underwater communications systems, see Category 5, Part 1 - Telecommunications.
a.

Systems, equipment and components, specially designed or modified for submersible vehicles and designed to operate at depths exceeding 1,000 m, as follows:

1.

Pressure housings or pressure hulls with a maximum inside chamber diameter exceeding 1,5 m;

2.

Direct current propulsion motors or thrusters;

3.

Umbilical cables, and connectors therefor, using optical fibre and having synthetic strength members;

4.

Components manufactured from material specified in 8C001;

Underwater vision systems as follows:

Remotely controlled articulated manipulators specially designed or modified for use with submersible vehicles and having any of the following:

Air independent power systems specially designed for underwater use, as follows:

Propellers, power transmission systems, power generation systems and noise reduction systems, as follows:

Note 1: 8A002.r. does not control diver deterrent systems based on underwater explosive devices, air guns or combustible sources.
Note 2: 8A002.r. includes diver deterrent acoustic systems that use spark gap sources, also known as plasma sound sources.
[8B] Test, Inspection and Production Equipment

[8B001] Water tunnels having a background noise of less than 100 dB (reference 1 μPa, 1 Hz), in the frequency range from 0 to 500 Hz and designed for measuring acoustic fields generated by a hydro-flow around propulsion system models.

[8C] Materials

[8C001] 'Syntactic foam' designed for underwater use and having all of the following:

N.B.: See also 8A002.a.4.
a.

Designed for marine depths exceeding 1 000 m; and

b.

A density less than 561 kg/m3.

Technical Note:

'Syntactic foam' consists of hollow spheres of plastic or glass embedded in a resin matrix.

[8D] Software

[8D001] "Software" specially designed or modified for the "development", "production" or "use" of equipment or materials, specified in 8A, 8B or 8C.

[8D002] Specific "software" specially designed or modified for the "development", "production", repair, overhaul or refurbishing (re-machining) of propellers specially designed for underwater noise reduction.

[8E] Technology

[8E001] "Technology" according to the General Technology Note for the "development" or "production" of equipment or materials, specified in 8A, 8B or 8C.

[8E002] Other "technology" as follows:

a.

"Technology" for the "development", "production", repair, overhaul or refurbishing (re-machining) of propellers specially designed for underwater noise reduction;

b.

"Technology" for the overhaul or refurbishing of equipment specified in 8A001, 8A002.b., 8A002.j., 8A002.o. or 8A002.p.

CATEGORY 9 — AEROSPACE AND PROPULSION
[9A] Systems, Equipment and Components
N.B.: For propulsion systems designed or rated against neutron or transient ionizing radiation, see the Military Goods Controls.

[9A001] Aero gas turbine engines having any of the following:

N.B.: SEE ALSO 9A101.

[9A002] 'Marine gas turbine engines' with an ISO standard continuous power rating of 24 245 kW or more and a specific fuel consumption not exceeding 0.219 kg/kWh in the power range from 35 to 100 %, and specially designed assemblies and components therefor.

Note: The term 'marine gas turbine engines' includes those industrial, or aero-derivative, gas turbine engines adapted for a ship's electric power generation or propulsion.

[9A003] Specially designed assemblies or components, incorporating any of the "technologies" specified in 9E003.a., 9E003.h. or 9E003i., for any of the following aero gas turbine engines:

a.

Specified in 9A001; or

b.

Whose design or production origins are either non- EU Member States or Wassenaar Arrangement Participating States;or unknown to the manufacturer.

[9A004] [X1Space launch vehicles, "spacecraft", "spacecraft buses", "spacecraft payloads", "spacecraft" on-board systems or equipment, and terrestrial equipment, as follows

N.B.: SEE ALSO 9A104.
a.

Space launch vehicles;

b.

"Spacecraft";

c.

"Spacecraft buses";

9A004

( continued )

d.

"Spacecraft payloads" incorporating items specified in 3A001.b.1.a.4., 3A002.g., 5A001.a.1., 5A001.b.3., 5A002.a.5., 5A002.a.9., 6A002.a.1., 6A002.a.2., 6A002.b., 6A002.d., 6A003.b., 6A004.c., 6A004.e., 6A008.d., 6A008.e., 6A008.k., 6A008.l. or 9A010.c.;

e.

On-board systems or equipment, specially designed for "spacecraft" and having any of the following functions:

[9A005] Liquid rocket propulsion systems containing any of the systems or components, specified in 9A006.

N.B.: SEE ALSO 9A105 AND 9A119.

[9A006] Systems and components, specially designed for liquid rocket propulsion systems, as follows:

N.B.: SEE ALSO 9A106, 9A108 AND 9A120.
a.

Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems, specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30 % per year;

b.

Cryogenic containers or closed-cycle refrigeration systems, capable of providing temperatures of 100 K (– 173 °C) or less for "aircraft" capable of sustained flight at speeds exceeding Mach 3, launch vehicles or "spacecraft";

c.

Slush hydrogen storage or transfer systems;

d.

High pressure (exceeding 17,5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems;

e.

High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor;

f.

Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders);

g.

Liquid propellant injectors with individual orifices of 0,381 mm or smaller in diameter (an area of 1,14 × 10–3 cm2 or smaller for non-circular orifices) and specially designed for liquid rocket engines;

h.

One-piece carbon-carbon thrust chambers or one-piece carbon-carbon exit cones, with densities exceeding 1,4 g/cm3 and tensile strengths exceeding 48 MPa.

[9A007] Solid rocket propulsion systems having any of the following:

N.B.: SEE ALSO 9A107 AND 9A119.

[9A008] Components specially designed for solid rocket propulsion systems, as follows:

N.B.: SEE ALSO 9A108.

[9A009] Hybrid rocket propulsion systems having any of the following:

N.B.: SEE ALSO 9A109 AND 9A119.
a.

Total impulse capacity exceeding 1,1 MNs; or

b.

Thrust levels exceeding 220 kN in vacuum exit conditions.

[9A010] Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or "spacecraft", as follows:

N.B.: SEE ALSO 1A002 AND 9A110.

[9A011] Ramjet, scramjet or combined cycle engines, and specially designed components therefor.

N.B.: SEE ALSO 9A111 AND 9A118.

[9A012] "Unmanned aerial vehicles" ("UAVs"), unmanned "airships", related, equipment and components, as follows:

N.B.: SEE ALSO 9A112.
a.

"UAVs" or unmanned "airships", designed to have controlled flight out of the direct 'natural vision' of the 'operator' and having any of the following:

[9A101] Turbojet and turbofan engines, other than those specified in 9A001, as follows;

[9A102] 'Turboprop engine systems' specially designed for unmanned aerial vehicles specified in 9A012 or 9A112.a, and specially designed components therefor, having a 'maximum power' greater than 10 kW.

Note: 9A102 does not control civil certified engines.
Technical Notes:
1. For the purposes of 9A102 a 'turboprop engine system' incorporates all of the following:
a.

Turboshaft engine; and

b.

Power transmission system to transfer the power to a propeller.

2. For the purposes of 9A102 the 'maximum power' is achieved uninstalled at sea level static conditions using ICAO standard atmosphere.

[9A104] Sounding rockets, capable of a range of at least 300 km.

N.B.: SEE ALSO 9A004.

[9A105] Liquid propellant rocket engines, as follows:

N.B.: SEE ALSO 9A119.
a.

Liquid propellant rocket engines usable in "missiles", other than those specified in 9A005, integrated, or designed or modified to be integrated, into a liquid propellant propulsion system which has a total impulse capacity equal to or greater than 1.1 MNs;

b.

Liquid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., integrated, or designed or modified to be integrated, into a liquid propellant propulsion system which has a total impulse capacity equal to or greater than 0,841 MNs.

[9A106] Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion systems:

a.

Ablative liners for thrust or combustion chambers, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

b.

Rocket nozzles, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

[9A107] Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0,841 MNs.

N.B.: SEE ALSO 9A119.

[9A108] Components, other than those specified in 9A008, as follows, specially designed for solid rocket propulsion systems:

[9A109] Hybrid rocket motors and specially designed components as follows:

a.

Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor;

b.

Specially designed components for hybrid rocket motors specified in 9A009 that are usable in "missiles".

N.B.: SEE ALSO 9A009 and 9A119.

[9A110] Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in 'missiles' or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.

N.B.: SEE ALSO 1A002.
Technical Note:

In 9A110 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[9A111] Pulse jet engines, usable in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor.

N.B.: SEE ALSO 9A011 AND 9A118.

[9A112] "Unmanned aerial vehicles" ("UAVs"), other than those specified in 9A012, as follows:

a.

"Unmanned aerial vehicles" ("UAVs") capable of a range of 300 km;

b.

"Unmanned aerial vehicles" ("UAVs") having all of the following:

1.

Having any of the following:

a.

An autonomous flight control and navigation capability; or

b.

Capability of controlled flight out of the direct vision range involving a human operator; and

2.

Having any of the following:

a.

Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or

b.

Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres.

Technical Notes:
1. An aerosol consists of particulate or liquids other than fuel components, by products or additives, as part of the "payload" to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding.
2. An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream.

[9A115] Launch support equipment as follows:

a.

Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or unmanned aerial vehicles specified in 9A012 or 9A112.a.;

b.

Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

[9A116] Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows:

a.

Reentry vehicles;

b.

Heat shields and components therefor, fabricated of ceramic or ablative materials;

c.

Heat sinks and components therefor, fabricated of light-weight, high heat capacity materials;

d.

Electronic equipment specially designed for reentry vehicles.

[9A117] Staging mechanisms, separation mechanisms, and interstages, usable in "missiles".

N.B.: SEE ALSO 9A121.

[9A118] Devices to regulate combustion usable in engines, which are usable in "missiles" or unmanned aerial vehicles specified in 9A012, or 9A112.a., specified in 9A011 or 9A111.

[9A119] Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.

[9A120] Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or 'other liquid propellants', used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km.

Note: In 9A120 'other liquid propellants' includes, but is not limited to, propellants specified in the Military Goods Controls.

[9A121] Umbilical and interstage electrical connectors specially designed for "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

Technical Note:

Interstage connectors referred to in 9A121 also include electrical connectors installed between the "missile", space launch vehicle or sounding rocket and their payload.

[9A350] Spraying or fogging systems, specially designed or modified for fitting to aircraft, "lighter-than-air vehicles" or unmanned aerial vehicles, and specially designed components therefor, as follows:

a.

Complete spraying or fogging systems capable of delivering, from a liquid suspension, an initial droplet 'VMD' of less than 50 μm at a flow rate of greater than two litres per minute;

b.

Spray booms or arrays of aerosol generating units capable of delivering, from a liquid suspension, an initial droplet 'VMD' of less than 50 μm at a flow rate of greater than two litres per minute;

c.

Aerosol generating units specially designed for fitting to systems specified in 9A350.a. and b.

Note: Aerosol generating units are devices specially designed or modified for fitting to aircraft such as nozzles, rotary drum atomizers and similar devices.
[9B] Test, Inspection and Production Equipment

[9B001] Equipment, tooling or fixtures, specially designed for manufacturing gas turbine blades, vanes or "tip shroud" castings, as follows:

a.

Directional solidification or single crystal casting equipment;

b.

Cores or shells (moulds), specially designed for casting, manufactured from refractory metals or ceramics;

c.

Directional-solidification or single-crystal additive-manufacturing equipment.

[9B002] On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, having all of the following:

a.

Specially designed for the "development" of gas turbine engines, assemblies or components; and

b.

Incorporating "technology" specified in 9E003.h. or 9E003.i.

[9B003] Equipment specially designed for the "production" or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.

[9B004] Tools, dies or fixtures, for the solid state joining of "superalloy", titanium or intermetallic airfoil-to-disk combinations described in 9E003.a.3. or 9E003.a.6. for gas turbines.

[9B005] On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following:

N.B.: SEE ALSO 9B105.

[9B006] Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 μPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1 273 K (1 000 °C), and specially designed quartz heaters therefor.

N.B.: SEE ALSO 9B106.

[9B007] Equipment specially designed for inspecting the integrity of rocket motors and using Non-Destructive Test (NDT) techniques other than planar x-ray or basic physical or chemical analysis.

[9B008] Direct measurement wall skin friction transducers specially designed to operate at a test flow total (stagnation) temperature exceeding 833 K (560 °C).

[9B009] Tooling specially designed for producing turbine engine powder metallurgy rotor components capable of operating at stress levels of 60 % of Ultimate Tensile Strength (UTS) or more and metal temperatures of 873 K (600 °C) or more.

[9B010] Equipment specially designed for the production of items specified in 9A012.

[9B105] 'Aerodynamic test facilities' for speeds of Mach 0,9 or more, usable for 'missiles' and their subsystems.

N.B.: SEE ALSO 9B005.
Note: 9B105 does not control wind-tunnels for speeds of Mach 3 or less with dimension of the 'test cross section size' equal to or less than 250 mm.
Technical Note:
1. In 9B105 'aerodynamic test facilities' includes wind tunnels and shock tunnels for the study of airflow over objects.
2. In Note to 9B105, 'test cross section size' means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest 'test cross section' location. 'Test cross section' is the section perpendicular to the flow direction.
3. In 9B105 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[9B106] Environmental chambers and anechoic chambers, as follows:

a.

Environmental chambers capable of simulating all the following flight conditions:

1.

Having any of the following:

a.

Altitude equal to or greater than 15 km; or

b.

Temperature range from below 223 K (– 50 °C) to above 398 K (+ 125 °C); and

2.

Incorporating, or 'designed or modified' to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured 'bare table', between 20 Hz and 2 kHz while imparting forces equal to or greater than 5 kN;

[9B115] Specially designed "production equipment" for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.

[9B116] Specially designed "production facilities" for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or 'missiles'.

Technical Note:

In 9B116 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[9B117] Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:

a.

The capacity to handle more than 68 kN of thrust; or

b.

Capable of simultaneously measuring the three axial thrust components.

[9C] Materials

[9C108] "Insulation" material in bulk form and "interior lining", other than those specified in 9A008, for rocket motor cases usable in "missiles" or specially designed for 'missiles'.

Technical Note:

In 9C108 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[9C110] Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a "specific tensile strength" greater than 7,62 × 104 m and a "specific modulus" greater than 3,18 × 106 m.

N.B.: SEE ALSO 1C010 AND 1C210.
Note: The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (Tg), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent.
[9D] Software

[9D001] "Software" specially designed or modified for the "development" of equipment or "technology", specified in 9A001 to 9A119, 9B or 9E003.

[9D002] "Software" specially designed or modified for the "production" of equipment specified in 9A001 to 9A119 or 9B.

[9D003] "Software" incorporating "technology" specified in 9E003.h. and used in "FADEC Systems" for systems specified in 9A or equipment specified in 9B.

[9D004] Other "software" as follows:

a.

2D or 3D viscous "software", validated with wind tunnel or flight test data required for detailed engine flow modelling;

b.

"Software" for testing aero gas turbine engines, assemblies or components, specially designed to collect, reduce and analyse data in real time and capable of feedback control, including the dynamic adjustment of test articles or test conditions, as the test is in progress;

c.

"Software" specially designed to control directional solidification or single crystal material growth in equipment specified in 9B001.a. or 9B001.c.;

d.

Not used;

e.

"Software" specially designed or modified for the operation of items specified in 9A012;

f.

"Software" specially designed to design the internal cooling passages of aero gas turbine blades, vans and "tip shrouds";

g.

"Software" having all of the following:

1.

Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and

2.

Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions, which have been validated with actual aero gas turbine engine (experimental or production) performance data.

[9D005] "Software" specially designed or modified for the operation of items specified in 9A004.e. or 9A004.f.

[9D101] "Software" specially designed or modified for the "use" of goods specified in 9B105, 9B106, 9B116 or 9B117.

[9D103] "Software" specially designed for modelling, simulation or design integration of the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104, or "missiles" or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.

Note: "Software" specified in 9D103 remains controlled when combined with specially designed hardware specified in 4A102.

[9D104] "Software" specially designed or modified for the "use" of goods specified in 9A001, 9A005, 9A006.d., 9A006.g., 9A007.a., 9A008.d., 9A009.a., 9A010.d., 9A011, 9A101, 9A102, 9A105, 9A106.c., 9A106.d., 9A107, 9A108.c., 9A109, 9A111, 9A115.a., 9A116.d., 9A117 or 9A118.

[9D105] "Software" which coordinates the function of more than one subsystem, other than that specified in 9D003.e.specially designed or modified for "use" in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.or 'missiles'

Technical Note:

In 9D105 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

[9E] Technology
Note: "Development" or "production" "technology" specified in 9E001 to 9E003 for gas turbine engines remains controlled when used for repair or overhaul. Excluded from control are: technical data, drawings or documentation for maintenance activities directly associated with calibration, removal or replacement of damaged or unserviceable line replaceable units, including replacement of whole engines or engine modules.

[9E001] "Technology" according to the General Technology Note for the "development" of equipment or "software", specified in 9A001.b., 9A004 to 9A012, 9A350, 9B or 9D.

[9E002] "Technology" according to the General Technology Note for the "production" of equipment specified in 9A001.b., 9A004 to 9A011, 9A350 or 9B.

N.B.: For "technology" for the repair of controlled structures, laminates or materials, see 1E002.f.

[9E003] Other "technology" as follows:

a.

"Technology" "required" for the "development" or "production" of any of the following gas turbine engine components or systems:

1.

Gas turbine blades, vanes or "tip shrouds", made from directionally solidified (DS) or single crystal (SC) alloys and having (in the 001Miller Index Direction) a stress-rupture life exceeding 400 hours at 1,273 K (1 000 °C) at a stress of 200 MPa, based on the average property values;

2.

Combustors having any of the following:

a.

Thermally decoupled liners designed to operate at 'combustor exit temperature' exceeding 1 883 K (1 610 °C);

b.

Non-metallic liners;

c.

Non-metallic shells; or

Components that are any of the following:

"Technology" "required" for manufacturing cooling holes, in gas turbine engine components incorporating any of the "technologies" specified by 9E003.a.1., 9E003.a.2. or 9E003.a.5., and having any of the following:

Having all of the following:

Note: 9E003.c. does not control "technology" for manufacturing constant radius cylindrical holes that are straight through and enter and exit on the external surfaces of the component.

"Technology" for the "development" or "production" of reciprocating diesel engine ground vehicle propulsion systems having all of the following:

"Technology" "required" for the "development" or "production" of 'high output diesel engines' for solid, gas phase or liquid film (or combinations thereof) cylinder wall lubrication and permitting operation to temperatures exceeding 723 K (450 °C), measured on the cylinder wall at the top limit of travel of the top ring of the piston;

"Technology" for gas turbine engine "FADEC systems" as follows:

[9E101]

[9E102] "Technology" according to the General Technology Note for the "use" of space launch vehicles specified in 9A004, goods specified in 9A005 to 9A011, 'UAV's specified in 9A012 or goods specified in 9A101, 9A102, 9A104 to9A111,9A112.a., 9A115 to 9A121, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101 or 9D103.

Technical Note:

In 9E102 'UAV' means unmanned aerial vehicle systems capable of a range exceeding 300 km.

ANNEX IIU.K.

ANNEX IIaU.K. UNION GENERAL EXPORT AUTHORISATION NO EU001 (referred to in Article 9(1) of this Regulation)

Exports to Australia, Canada, Japan, New Zealand, Norway, Switzerland, including Liechtenstein, and United States of America

Issuing authority: European Commission
Part 1 U.K.

This general export authorisation covers all dual-use items specified in any entry in Annex I to this Regulation, except those listed in Annex IIg.

Part 2 U.K.

This export authorisation is valid throughout the Union for exports to the following destinations:

  • Australia

  • Canada

  • Japan

  • New Zealand

  • Norway

  • Switzerland, including Lichtenstein

  • United States of America

Conditions and requirements for use of this authorisation
1.Exporters that use this authorisation shall notify the competent authorities of the Member State where they are established of their first use of this authorisation no later than 30 days after the date when the first export took place.

Exporters shall also report in the Single Administrative Document the fact that they are using this authorisation EU 001 by indicating in box 44 the reference X002.

2.This authorisation may not be used if:
  • the exporter has been informed by the competent authorities of the Member State in which he is established that the items in question are or may be intended, in their entirety or in part, for use in connection with the development, production, handling, operation, maintenance, storage, detection, identification or dissemination of chemical, biological or nuclear weapons or other nuclear explosive devices or the development, production, maintenance or storage of missiles capable of delivering such weapons, or if the exporter is aware that the items in question are intended for such use;

  • the exporter has been informed by the competent authorities of the Member State in which he is established that the items in question are or may be intended for a military end use as defined in Article 4(2) of this Regulation in a country subject to an arms embargo imposed by a decision or a common position adopted by the Council or a decision of the OSCE or an arms embargo imposed by a binding resolution of the Security Council of the United Nations, or if the exporter is aware that the items in question are intended for the above mentioned uses;

  • the relevant items are exported to a customs free zone or free warehouse which is located in a destination covered by this authorisation.

3.Reporting requirements attached to the use of this authorisation and the additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States.

A Member State may require the exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within ten working days of receipt.

Where applicable the requirements set out in the first two paragraphs of this point shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations.

ANNEX IIbU.K. UNION GENERAL EXPORT AUTHORISATION No EU002 (referred to in Article 9(1) of this Regulation)

Exports of certain dual-use items to certain destinations

Issuing authority: European Union
Part 1 — U.K. Items

This general export authorisation covers the following dual-use items specified in Annex I to this Regulation:

  • 1A001,

  • 1A003,

  • 1A004,

  • 1C003b-c,

  • 1C004,

  • 1C005,

  • 1C006,

  • 1C008,

  • 1C009,

  • 2B008,

  • 3A001a3,

  • 3A001a6-12,

  • 3A002c-f,

  • 3C001,

  • 3C002,

  • 3C003,

  • 3C004,

  • 3C005,

  • 3C006.

Part 2 — U.K. Destinations

This authorisation is valid throughout the Union for exports to the following destinations:

  • Argentina,

  • Croatia,

  • Iceland,

  • South Africa,

  • South Korea,

  • Turkey.

Part 3 — U.K. Conditions and requirements for use
1.This authorisation does not authorise the export of items where:
(1)

the exporter has been informed by the competent authorities of the Member State in which he is established as defined in Article 9(6) of this Regulation that the items in question are or may be intended, in their entirety or in part:

(a)

for use in connection with the development, production, handling, operation, maintenance, storage, detection, identification or dissemination of chemical, biological or nuclear weapons or other nuclear explosive devices, or the development, production, maintenance or storage of missiles capable of delivering such weapons;

(b)

for a military end-use as defined in Article 4(2) of this Regulation in a country subject to an arms embargo imposed by a decision or a common position adopted by the Council or a decision of the Organisation for Security and Cooperation in Europe or an arms embargo imposed by a binding resolution of the Security Council of the United Nations; or

(c)

for use as parts or components of military items listed in national military lists that have been exported from the territory of the Member State concerned without authorisation or in breach of an authorisation prescribed by the national legislation of that Member State;

(2)

the exporter, under his obligation to exercise due diligence, is aware that the items in question are intended, in their entirety or in part, for any of the uses referred to in subparagraph (1);

(3)

the relevant items are exported to a customs-free zone or a free warehouse which is located in a destination covered by this authorisation.

2.Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU002 in box 44 of the Single Administrative Document.
3.Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.

Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States.

A Member State may require the exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation.

Where applicable the requirements set out in the second and third paragraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations.

ANNEX IIcU.K. UNION GENERAL EXPORT AUTHORISATION No EU003 (referred to in Article 9(1) of this Regulation)

Export after repair/replacement

Issuing authority: European Union
Part 1 — U.K. Items
1.This general export authorisation covers all dual-use items specified in any entry in Annex I to this Regulation except those listed in paragraph 2 where:
(a)

the items were reimported into the customs territory of the European Union for the purpose of maintenance, repair or replacement, and are exported or re-exported to the country of consignment without any changes to their original characteristics within a period of 5 years after the date when the original export authorisation has been granted; or

(b)

the items are exported to the country of consignment in exchange for items of the same quality and number which were reimported into the customs territory of the European Union for maintenance, repair or replacement within a period of 5 years after the date when the original export authorisation has been granted.

2.Items excluded:
(a)

all items listed in Annex IIg;

(b)

all items in Sections D and E set out in Annex I to this Regulation;

(c)

the following items specified in Annex I to this Regulation:

  • 1A002a,

  • 1C012a,

  • 1C227,

  • 1C228,

  • 1C229,

  • 1C230,

  • 1C231,

  • 1C236,

  • 1C237,

  • 1C240,

  • 1C350,

  • 1C450,

  • 5A001b5,

  • 5A002a2 to 5A002a9,

  • 6A001a2a1,

  • 6A001a2a5,

  • 6A002a1c,

  • 8A001b,

  • 8A001d,

  • 9A011.

Part 2 — U.K. Destinations

This authorisation is valid throughout the Union for exports to the following destinations:

  • Albania

  • Argentina

  • Bosnia and Herzegovina

  • Brazil

  • Chile

  • China (including Hong Kong and Macao)

  • Croatia

  • former Yugoslav Republic of Macedonia, the

  • French Overseas Territories

  • Iceland

  • India

  • Kazakhstan

  • Mexico

  • Montenegro

  • Morocco

  • Russia

  • Serbia

  • Singapore

  • South Africa

  • South Korea

  • Tunisia

  • Turkey

  • Ukraine

  • United Arab Emirates

Part 3 — U.K. Conditions and requirements for use
1.This authorisation can only be used when the initial export has taken place under a Union General Export Authorisation or an initial export authorisation has been granted by the competent authorities of the Member State where the original exporter was established for the export of the items which have subsequently been reimported into the customs territory of the European Union for the purposes of maintenance, repair or replacement. This authorisation is valid only for exports to the original end-user.
2.This authorisation does not authorise the export of items where:
(1)

the exporter has been informed by the competent authorities of the Member State in which he is established as defined in Article 9(6) of this Regulation that the items in question are or may be intended, in their entirety or in part,

(a)

for use in connection with the development, production, handling, operation, maintenance, storage, detection, identification or dissemination of chemical, biological or nuclear weapons or other nuclear explosive devices or the development, production, maintenance or storage of missiles capable of delivering such weapons;

(b)

for a military end-use as defined in Article 4(2) of this Regulation where the purchasing country or country of destination is subject to an arms embargo imposed by a decision or a common position adopted by the Council or a decision of the Organisation for Security and Cooperation in Europe or an arms embargo imposed by a binding resolution of the Security Council of the United Nations; or

(c)

for use as parts or components of military items listed in the national military list that have been exported from the territory of the Member State concerned without authorisation or in breach of an authorisation prescribed by the national legislation of that Member State;

(2)

the exporter is aware that the items in question are intended, in their entirety or in part, for any of the uses referred to in subparagraph (1);

(3)

the relevant items are exported to a customs-free zone or a free warehouse which is located in a destination covered by this authorisation;

(4)

the initial authorisation has been annulled, suspended, modified or revoked;

(5)

the exporter, under his obligation to exercise due diligence, is aware that the end-use of the items in question is different from that specified in the original export authorisation.

3.On exportation of any of the items pursuant to this authorisation, exporters must:
(1)

mention the reference number of the initial export authorisation in the export declaration to customs together with the name of the Member State that granted the authorisation, the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU003 in box 44 of the Single Administrative Document;

(2)

provide customs officers, if so requested, with documentary evidence of the date of importation of the items into the Union, of any maintenance, repair or replacement of the items carried out in the Union and of the fact that the items are being returned to the end-user and the country from which they were imported into the Union.

4.Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.

Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States.

A Member State may require the exporter established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation.

Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations.

5.This authorisation covers items for 'repair', 'replacement' and 'maintenance'. This may involve coincidental improvement on the original goods, e.g. resulting from the use of modern spare parts or from use of a later built standard for reliability or safety reasons, provided that this does not result in any enhancement to the functional capability of the items or provide the items with new or additional functions.

ANNEX IIdU.K. UNION GENERAL EXPORT AUTHORISATION No EU004 (referred to in Article 9(1) of this Regulation)

Temporary export for exhibition or fair

Issuing authority: European Union
Part 1 — U.K. Items

This general export authorisation covers all dual-use items specified in any entry in Annex I to this Regulation except:

(a)

all items listed in Annex IIg;

(b)

all items in Section D set out in Annex I to this Regulation (this does not include software necessary to the proper functioning of the equipment for the purpose of the demonstration);

(c)

all items in Section E set out in Annex I to this Regulation;

(d)

the following items specified in Annex I to this Regulation:

  • 1A002a,

  • 1C002.b.4,

  • 1C010,

  • 1C012.a,

  • 1C227,

  • 1C228,

  • 1C229,

  • 1C230,

  • 1C231,

  • 1C236,

  • 1C237,

  • 1C240,

  • 1C350,

  • 1C450,

  • 5A001b5,

  • 5A002a2 to 5A002a9,

  • 6A001,

  • 6A002a,

  • 6A008l3,

  • 8A001b,

  • 8A001d,

  • 9A011.

Part 2 — U.K. Destinations

This authorisation is valid throughout the Union for exports to the following destinations:

Albania, Argentina, Bosnia and Herzegovina, Brazil, Chile, China (including Hong Kong and Macao), Croatia, the former Yugoslav Republic of Macedonia, French Overseas Territories, Iceland, India, Kazakhstan, Mexico, Montenegro, Morocco, Russia, Serbia, Singapore, South Africa, South Korea, Tunisia, Turkey, Ukraine, and United Arab Emirates.

Part 3 — U.K. Conditions and requirements for use
1.This authorisation authorises the export of items listed in Part 1 on condition that the export concerns temporary export for exhibition or fair as defined in point 6 and that the items are reimported within a period of 120 days after the initial export, complete and without modification, into the customs territory of the European Union.
2.The competent authority of the Member State where the exporter is established as defined in Article 9(6) of this Regulation may, at the exporter’s request, waive the requirement that the items are to be reimported as stated in paragraph 1. To waive the requirement, the procedure for individual authorisations laid down in Articles 9(2) and 14(1) of this Regulation shall apply accordingly.
3.This authorisation does not authorise the export of items where:
(1)

the exporter has been informed by the competent authorities of the Member State in which he is established that the items in question are or may be intended, in their entirety or in part:

(a)

for use in connection with the development, production, handling, operation, maintenance, storage, detection, identification or dissemination of chemical, biological or nuclear weapons or other nuclear explosive devices, or the development, production, maintenance or storage of missiles capable of delivering such weapons;

(b)

for a military end-use as defined in Article 4(2) of this Regulation where the purchasing country or country of destination is subject to an arms embargo imposed by a decision or a common position adopted by the Council or a decision of the Organisation for Security and Cooperation in Europe or an arms embargo imposed by a binding resolution of the Security Council of the United Nations; or

(c)

for use as parts or components of military items listed in the national military list that have been exported from the territory of the Member State concerned without authorisation or in breach of an authorisation prescribed by the national legislation of that Member State;

(2)

the exporter is aware that the items in question are intended, in their entirety or in part, for any of the uses referred to in subparagraph (1);

(3)

the relevant items are exported to a customs-free zone or a free warehouse which is located in a destination covered by this authorisation;

(4)

the exporter has been informed by a competent authority of the Member State in which he is established, or is otherwise aware (e.g. from information received from the manufacturer), that the items in question have been classified by the competent authority as having a protective national security classification marking, equivalent to or above CONFIDENTIEL UE/EU CONFIDENTIAL;

(5)

their return, in their original state, without the removal, copying or dissemination of any component or software, cannot be guaranteed by the exporter, or where a transfer of technology is connected with a presentation;

(6)

the relevant items are to be exported for a private presentation or demonstration (e.g. in in-house showrooms);

(7)

the relevant items are to be merged into any production process;

(8)

the relevant items are to be used for their intended purpose, except to the minimum extent required for effective demonstration, but without making specific test outputs available to third parties;

(9)

the export is to take place as a result of a commercial transaction, in particular as regards the sale, rental or lease of the relevant items;

(10)

the relevant items are to be stored at an exhibition or fair only for the purpose of sale, rent or lease, without being presented or demonstrated;

(11)

the exporter makes any arrangement which would prevent him from keeping the relevant items under his control during the whole period of the temporary export.

4.Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU004 in box 44 of the Single Administrative Document.
5.Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.

Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States.

A Member State may require exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation.

Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations.

6.For the purpose of this authorisation, 'exhibition or fair' means commercial events of a specific duration at which several exhibitors make demonstrations of their products to trade visitors or to the general public.

ANNEX IIeU.K. UNION GENERAL EXPORT AUTHORISATION NO EU005 (referred to in Article 9(1) of this Regulation)

Telecommunications

Issuing authority: European Union
Part 1 — U.K. Items

This general export authorisation covers the following dual-use items specified in Annex I to this Regulation:

(a)

the following items of Category 5, Part l:

(i)

items, including specially designed or developed components and accessories therefor specified in 5A001b2 and 5A001c and d;

(ii)

items specified in 5B001 and 5D001, where test, inspection and production equipment is concerned and software for items mentioned under (i);

(b)

technology controlled by 5E001a, where required for the installation, operation, maintenance or repair of items specified under (a) and intended for the same end-user.

Part 2 — U.K. Destinations

This authorisation is valid throughout the Union for exports to the following destinations:

Argentina, China (including Hong Kong and Macao), Croatia, India, Russia, South Africa, South Korea, Turkey, and Ukraine.

Part 3 — U.K. Conditions and requirements for use
1.This authorisation does not authorise the export of items where:
(1)

the exporter has been informed by the competent authorities of the Member State in which he is established as defined in Article 9(6) of this Regulation that the items in question are or may be intended, in their entirety or in part:

(a)

for use in connection with the development, production, handling, operation, maintenance, storage, detection, identification or dissemination of chemical, biological or nuclear weapons or other nuclear explosive devices, or the development, production, maintenance or storage of missiles capable of delivering such weapons;

(b)

for a military end-use as defined in Article 4(2) of this Regulation where the purchasing country or country of destination is subject to an arms embargo imposed by a decision or a common position adopted by the Council or a decision of the Organisation for Security and Cooperation in Europe or an arms embargo imposed by a binding resolution of the Security Council of the United Nations;

(c)

for use as parts or components of military items listed in the national military list that have been exported from the territory of the Member State concerned without authorisation or in breach of an authorisation prescribed by the national legislation of that Member State; or

(d)

for use in connection with a violation of human rights, democratic principles or freedom of speech as defined by the Charter of Fundamental Rights of the European Union, by using interception technologies and digital data transfer devices for monitoring mobile phones and text messages and targeted surveillance of Internet use (e.g. via Monitoring Centres and Lawful Interception Gateways);

(2)

the exporter, under his obligation to exercise due diligence, is aware that the items in question are intended, in their entirety or in part, for any of the uses referred to in subparagraph 1;

(3)

the exporter, under his obligation to exercise due diligence, is aware that the items in question will be re-exported to any destination other than those listed in Part 2 of this Annex or in Part 2 of Annex IIa or to Member States;

(4)

the relevant items are exported to a customs-free zone or a free warehouse which is located in a destination covered by this authorisation.

2.Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU005 in box 44 of the Single Administrative Document.
3.Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.

Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States.

A Member State may require exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation.

Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations.

ANNEX IIfU.K. UNION GENERAL EXPORT AUTHORISATION No EU006 (referred to in Article 9(1) of this Regulation)

Chemicals

Part 1 — U.K. Items

This general export authorisation covers the following dual-use items specified in Annex I to this Regulation:

  • 1C350:

    1.

    Thiodiglycol (111-48-8);

    2.

    Phosphorus oxychloride (10025-87-3);

    3.

    Dimethyl methylphosphonate (756-79-6);

    5.

    Methylphosphonyl dichloride (676-97-1);

    6.

    Dimethyl phosphite (DMP) (868-85-9);

    7.

    Phosphorus trichloride (7719-12-2);

    8.

    Trimethyl phosphite (TMP) (121-45-9);

    9.

    Thionyl chloride (7719-09-7);

    10.

    3-Hydroxy-1-methylpiperidine (3554-74-3);

    11.

    N,N-Diisopropyl-(beta)-aminoethyl chloride (96-79-7);

    12.

    N,N-Diisopropyl-(beta)-aminoethane thiol (5842-07-9);

    13.

    Quinuclidin-3-ol (1619-34-7);

    14.

    Potassium fluoride (7789-23-3);

    15.

    2-Chloroethanol (107-07-3);

    16.

    Dimethylamine (124-40-3);

    17.

    Diethyl ethylphosphonate (78-38-6);

    18.

    Diethyl-N,N-dimethylphosphoramidate (2404-03-7);

    19.

    Diethyl phosphite (762-04-9);

    20.

    Dimethylamine hydrochloride (506-59-2);

    21.

    Ethyl phosphinyl dichloride (1498-40-4);

    22.

    Ethyl phosphonyl dichloride (1066-50-8);

    24.

    Hydrogen fluoride (7664-39-3);

    25.

    Methyl benzilate (76-89-1);

    26.

    Methyl phosphinyl dichloride (676-83-5);

    27.

    N,N-Diisopropyl-(beta)-amino ethanol (96-80-0);

    28.

    Pinacolyl alcohol (464-07-3);

    30.

    Triethyl phosphite (122-52-1);

    31.

    Arsenic trichloride (7784-34-1);

    32.

    Benzilic acid (76-93-7);

    33.

    Diethyl methylphosphonite (15715-41-0);

    34.

    Dimethyl ethylphosphonate (6163-75-3);

    35.

    Ethyl phosphinyl difluoride (430-78-4);

    36.

    Methyl phosphinyl difluoride (753-59-3);

    37.

    3-Quinuclidone (3731-38-2);

    38.

    Phosphorus pentachloride (10026-13-8);

    39.

    Pinacolone (75-97-8);

    40.

    Potassium cyanide (151-50-8);

    41.

    Potassium bifluoride (7789-29-9);

    42.

    Ammonium hydrogen fluoride or ammonium bifluoride (1341-49-7);

    43.

    Sodium fluoride (7681-49-4);

    44.

    Sodium bifluoride (1333-83-1);

    45.

    Sodium cyanide (143-33-9);

    46.

    Triethanolamine (102-71-6);

    47.

    Phosphorus pentasulphide (1314-80-3);

    48.

    Di-isopropylamine (108-18-9);

    49.

    Diethylaminoethanol (100-37-8);

    50.

    Sodium sulphide (1313-82-2);

    51.

    Sulphur monochloride (10025-67-9);

    52.

    Sulphur dichloride (10545-99-0);

    53.

    Triethanolamine hydrochloride (637-39-8);

    54.

    N,N-Diisopropyl-(Beta)-aminoethyl chloride hydrochloride (4261-68-1);

    55.

    Methylphosphonic acid (993-13-5);

    56.

    Diethyl methylphosphonate (683-08-9);

    57.

    N,N-Dimethylaminophosphoryl dichloride (677-43-0);

    58.

    Triisopropyl phosphite (116-17-6);

    59.

    Ethyldiethanolamine (139-87-7);

    60.

    O,O-Diethyl phosphorothioate (2465-65-8);

    61.

    O,O-Diethyl phosphorodithioate (298-06-6);

    62.

    Sodium hexafluorosilicate (16893-85-9);

    63.

    Methylphosphonothioic dichloride (676-98-2).

  • 1C450 a:

    4.

    Phosgene: Carbonyl dichloride (75-44-5);

    5.

    Cyanogen chloride (506-77-4);

    6.

    Hydrogen cyanide (74-90-8);

    7.

    Chloropicrin: Trichloronitromethane (76-06-2);

  • 1C450 b:

    1.

    Chemicals, other than those specified in the Military Goods Controls or in 1C350, containing a phosphorus atom to which is bonded one methyl, ethyl or propyl (normal or iso) group but not further carbon atoms;

    2.

    N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] phosphoramidic dihalides, other than N,N-Dimethylaminophosphoryl dichloride which is specified in 1C350.57;

    3.

    Dialkyl [methyl, ethyl or propyl (normal or iso)] N,N-dialkyl [methyl, ethyl or propyl (normal or iso)]-phosphoramidates, other than Diethyl-N,N-dimethylphosphoramidate which is specified in 1C350;

    4.

    N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethyl-2-chlorides and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethyl chloride or N,N-Diisopropyl-(beta)-aminoethyl chloride hydrochloride which are specified in 1C350;

    5.

    N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-ols and corresponding protonated salts; other than N,N-Diisopropyl-(beta)-aminoethanol (96-80-0) and N,N-Diethylaminoethanol (100-37-8) which are specified in 1C350;

    6.

    N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-thiols and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethane thiol which is specified in 1C350;

    8.

    Methyldiethanolamine (105-59-9).

Part 2 — U.K. Destinations

This authorisation is valid throughout the Union for exports to the following destinations:

Argentina, Croatia, Iceland, South Korea, Turkey, and Ukraine.

Part 3 — U.K. Conditions and requirements for use
1.This authorisation does not authorise the export of items where:
(1)

the exporter has been informed by the competent authorities of the Member State in which he is established as defined in Article 9(6) of this Regulation that the items in question are or may be intended, in their entirety or in part:

(a)

for use in connection with the development, production, handling, operation, maintenance, storage, detection, identification or dissemination of chemical, biological or nuclear weapons or other nuclear explosive devices, or the development, production, maintenance or storage of missiles capable of delivering such weapons;

(b)

for a military end-use as defined in Article 4(2) of this Regulation where the purchasing country or country of destination is subject to an arms embargo imposed by a decision or a common position adopted by the Council or a decision of the Organisation for Security and Cooperation in Europe or an arms embargo imposed by a binding resolution of the Security Council of the United Nations; or

(c)

for use as parts or components of military items listed in the national military list that have been exported from the territory of the Member State concerned without authorisation or in breach of an authorisation prescribed by the national legislation of that Member State;

(2)

the exporter, under his obligation to exercise due diligence, is aware that the items in question are intended, in their entirety or in part, for any of the uses referred to in subparagraph 1;

(3)

the exporter, under his obligation to exercise due diligence, is aware that the items in question will be re-exported to any destination other than those listed in Part 2 of this Annex or in Part 2 of Annex IIa or to Member States; or

(4)

the relevant items are exported to a customs-free zone or a free warehouse which is located in a destination covered by this authorisation.

2.Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU006 in box 44 of the Single Administrative Document.
3.Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.

Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States.

A Member State may require exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation.

Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations.

ANNEX IIgU.K. (List referred to in Article 9(4)(a) of this Regulation and Annexes IIa, IIc and IId to this Regulation)

The entries do not always provide a complete description of the items and the related notes in Annex I. Only Annex I provides a complete description of the items.

The mention of an item in this Annex does not affect the application of the General Software Note (GSN) in Annex I.

  • all items specified in Annex IV,

  • 0C001 'Natural uranium' or 'depleted uranium' or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing,

  • 0C002 'Special fissile materials' other than those specified in Annex IV,

  • 0D001 'Software' specially designed or modified for the 'development', 'production' or '…' of goods specified in Category 0, in so far as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV,

  • 0E001 'Technology' in accordance with the Nuclear Technology Note for the 'development', 'production' or '…' of goods specified in Category 0, in so far as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV,

  • 1A102 Resaturated pyrolised carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104,

  • 1C351 Human and animal pathogens and 'toxins',

  • 1C353 Genetic elements and genetically modified organisms,

  • 1C354 Plant pathogens,

  • 1C450a.1. amiton: O,O-Diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (78-53-5) and corresponding alkylated or protonated salts,

  • 1C450a.2. PFIB: 1,1,3,3,3-Pentafluoro-2-(trifluoromethyl)-1-propene (382-21-8),

  • 7E104 'Technology' for the integration of flight control, guidance and propulsion data into a flight management system for optimisation of rocket system trajectory,

  • 9A009.a. Hybrid rocket propulsion systems with total impulse capacity exceeding 1.1 MNs,

  • 9A117 Staging mechanisms, separation mechanisms and interstages usable in 'missiles.'

ANNEX IIIU.K.

'ANNEX IVU.K. (List referred to in Article 22(1) of this Regulation)

The entries do not always cover the complete description of the item and the related notes in Annex I (3) . Only Annex I provides for the complete description of the items.

The mention of an item in this Annex does not affect the application of the provisions concerning mass-market products in Annex I.

PART IU.K. (possibility of National General Authorisation for intra-Community trade)

Items of stealth technology
1C001

Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers.

1C101

Materials or devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures; other than those specified in 1C001, usable in "missiles", "missile" subsystems or unmanned aerial vehicles specified in 9A012.

1D103"Software" specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.
1E101"Technology" according to the GTN for the "use" of goods specified in 1C101 or 1D103.
1E102"Technology" according to the GTN for the "development" of "software" specified in 1D103.
6B008

Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less and specially designed components therefor.

6B108Systems specially designed for radar cross section measurement usable for "missiles" and their subsystems.
Items of the Community strategic control
1A007

Equipment and devices, specially designed to initiate charges and devices containing energetic materials, by electrical means, as follows:

1C239High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8 000 m/s.
1E201"Technology" according to the General Technology Note for the "use" of goods specified in 1C239.
3A229

High-current pulse generators, as follows …

3A232

Multipoint initiation systems, other than those specified in 1A007 above , as follows …

3E201"Technology" according to the General Technology Note for the "use" of equipment specified in 3A228.a., 3A228.b. or 3A231.
6A001Acoustics, limited to the following:
6A001.a.1.b.

Object detection or location systems having any of the following:

1.

A transmitting frequency below 5 kHz;

6.

Designed to withstand …;

6A001.a.2.a.2.Hydrophones … Incorporating …
6A001.a.2.a.3.Hydrophones … Having any …
6A001.a.2.a.6.Hydrophones … Designed for …
6A001.a.2.b.Towed acoustic hydrophone arrays …
6A001.a.2.c.Processing equipment, specially designed for real time application with towed acoustic hydrophone arrays, having "user-accessible programmability" and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beamforming using Fast Fourier or other transforms or processes;
6A001.a.2.e.

Bottom or bay cable systems having any of the following:

1.

Incorporating hydrophones …, or

2.

Incorporating multiplexed hydrophone group signal modules …;

6A001.a.2.f.Processing equipment, specially designed for real time application with bottom or bay cable systems, having "user-accessible programmability" and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beamforming using Fast Fourier or other transforms or processes;
6D003.a."Software" for the "real time processing" of acoustic data;
8A002.o.3.

Noise reduction systems designed for use on vessels of 1 000 tonnes displacement or more, as follows:

b.

Active noise reduction or cancellation systems, or magnetic bearings, specially designed for power transmission systems, and incorporating electronic control systems capable of actively reducing equipment vibration by the generation of anti-noise or anti-vibration signals directly to the source;

8E002.a."Technology" for the "development", "production", repair, overhaul or refurbishing (re-machining) of propellers specially designed for underwater noise reduction.
Items of the Community strategic control — Cryptography — Category 5 Part 2
5A002.a.2.

Equipment designed or modified to perform 'cryptanalytic functions'.

5D002.c.1Only software having the characteristics, or performing or simulating the functions, of equipment specified in 5A002.a.2.
5E002.a.Only "technology" for the "development", "production" or "use" of the goods specified in 5A002.a.2. or 5D002.c.1. above.
Items of the MTCR technology
7A117"Guidance sets", usable in "missiles" capable of achieving system accuracy of 3,33 % or less of the range (e.g., a "CEP" of 10 km or less at a range of 300 km), except "guidance sets" designed for missiles with a range under 300 km or manned aircraft .
7B001

Test, calibration or alignment equipment specially designed for equipment specified in 7A117 above.

7B003Equipment specially designed for the "production" of equipment specified in 7A117 above.
7B103"Production facilities" specially designed for equipment specified in 7A117 above .
7D101"Software" specially designed for the "use" of equipment specified in 7B003 or 7B103 above .
7E001"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 7A117, 7B003, 7B103 or 7D101 above .
7E002"Technology" according to the General Technology Note for the "production" of equipment specified in 7A117, 7B003 and 7B103 above .
7E101"Technology" according to the General Technology Note for the "use" of equipment specified in 7A117, 7B003, 7B103 and 7D101 above .
9A004

Space launch vehicles capable of delivering at least a 500 kg payload to a range of at least 300 km .

9A005

Liquid rocket propulsion systems containing any of the systems or components specified in 9A006 usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below .

9A007.a.

Solid rocket propulsion systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below , with any of the following:

9A008.d.

Components, as follows, specially designed for solid rocket propulsion systems:

9A104

Sounding rockets, capable of delivering at least a 500 kg payload to a range of at least 300 km.

9A105.a.

Liquid propellant rocket engines, as follows:

9A106.c.

Systems or components, other than those specified in 9A006, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems:

c.

Thrust vector control sub-systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km .

9A108.c.

Components, other than those specified in 9A008, usable in "missiles" as follows, specially designed for solid rocket propulsion systems:

c.

Thrust vector control sub-systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km .

9A116

Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows, except for reentry vehicles designed for non-weapon payloads:

a.

Reentry vehicles;

b.

Heat shields and components therefor fabricated of ceramic or ablative materials;

c.

Heat sinks and components therefor fabricated of light-weight, high heat capacity materials;

d.

Electronic equipment specially designed for reentry vehicles.

9A119Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of delivering at least a 500 kg payload to a range of 300 km, other than those specified in 9A005 or 9A007.a. above
9B115Specially designed "production equipment" for the systems, sub-systems and components specified in 9A005, 9A007.a., 9A008.d., 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above .
9B116Specially designed "production facilities" for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above .
9D101"Software" specially designed for the "use" of goods specified in 9B116 above .
9E001"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115, 9B116 or 9D101 above .
9E002

"Technology" according to the General Technology Note for the "production" of equipment specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115 or 9B116 above .

9E101"Technology" according to the General Technology Note for the "development" or "production" of goods specified in 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above .
9E102"Technology" according to the General Technology Note for the "use" of space launch vehicles specified in 9A004, 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116, 9A119, 9B115, 9B116 or 9D101 above .
Exemptions:

Annex IV does not control the following items of the MTCR technology:

1.

that are transferred on the basis of orders pursuant to a contractual relationship placed by the European Space Agency (ESA) or that are transferred by ESA to accomplish its official tasks;

2.

that are transferred on the basis of orders pursuant to a contractual relationship placed by a Member State's national space organisation or that are transferred by it to accomplish its official tasks;

3.

that are transferred on the basis of orders pursuant to a contractual relationship placed in connection with a Community space launch development and production programme signed by two or more European governments;

4.

that are transferred to a State-controlled space launching site in the territory of a Member State, unless that Member State controls such transfers within the terms of this Regulation.

PART IIU.K. (no National General Authorisation for intra-Community trade)

Items of the CWC (Chemical Weapons Convention)
1C351.d.4.Ricin
1C351.d.5.Saxitoxin
Items of the NSG technology

All Category 0 of Annex I is included in Annex IV, subject to the following:

  • 0C001: this item is not included in Annex IV.

  • 0C002: this item is not included in Annex IV, with the exception of special fissile materials as follows:

    (a)

    separated plutonium;

    (b)

    "uranium enriched in the isotopes 235 or 233" to more than 20 %.

  • 0C003 only if for use in a "nuclear reactor" (within 0A001.a)

  • 0D001 (software) is included in Annex IV except insofar as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV.

  • 0E001 (technology) is included in Annex IV except insofar as these related to 0C001 or to those items of 0C002 that are excluded from Annex IV.

1B226

Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.

1C012

Materials as follows:

1B231

Tritium facilities or plants, and equipment therefor, as follows:

a.

Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;

b.

Equipment for tritium facilities or plants, as follows:

1.

Hydrogen or helium refrigeration units capable of cooling to 23 K (– 250 °C) or less, with heat removal capacity greater than 150 W;

2.

Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.

1B233

Lithium isotope separation facilities or plants, and equipment therefor, as follows:

a.

Facilities or plants for the separation of lithium isotopes;

b.

Equipment for the separation of lithium isotopes, as follows:

1.

Packed liquid-liquid exchange columns specially designed for lithium amalgams;

2.

Mercury or lithium amalgam pumps;

3.

Lithium amalgam electrolysis cells;

4.

Evaporators for concentrated lithium hydroxide solution.

1C233

Lithium enriched in the lithium-6 (6Li) isotope to greater than its natural isotopic abundance, and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.

1C235

Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, and products or devices containing any of the foregoing.

1E001"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 1C012.b.
1E201"Technology" according to the General Technology Note for the "use" of goods specified in 1B226, 1B231, 1B233, 1C233 or 1C235.
3A228

Switching devices, as follows:

a.

Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:

1.

Containing three or more electrodes;

2.

Anode peak voltage rating of 2,5 kV or more;

3.

Anode peak current rating of 100 A or more; and

4.

Anode delay time of 10 μs or less;

3A231

Neutron generator systems, including tubes, having both of the following characteristics:

a.

Designed for operation without an external vacuum system; and

b.

Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction

3E201"Technology" according to the General Technology Note for the "use" of equipment specified in 3A229 or 3A232.
6A203

Cameras and components, other than those specified in 6A003, as follows:

a.

Mechanical rotating mirror cameras, as follows, and specially designed components therefor:

1.

Framing cameras with recording rates greater than 225000 frames per second;

2.

Streak cameras with writing speeds greater than 0,5 mm per microsecond;

6A225

Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.

6A226

Pressure sensors, as follows:

a.

Manganin gauges for pressures greater than 10 GPa;

b.

Quartz pressure transducers for pressures greater than 10 GPa.'

(1)

[X1Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) or (2006) should consult the competent authorities of the Member State in which they are established.]

(2)

[X1Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) or (2006) should consult the competent authorities of the Member State in which they are established.]

(3)

The differences in the wordings/scopes between Annex I and Annex IV are indicated with bold italic text.