xmlns:atom="http://www.w3.org/2005/Atom"

SCHEDULE 1PROHIBITED GOODS

PART III

GROUP 3INDUSTRIAL GOODS

Interpretations, exclusions and definitions

1.  Where notes are included in any entry of this Group they are to be treated as part of the entry.

2.  This Group does not specify software which is either:

a.generally available to the public or

b.1.sold from stock at retail selling points, without restriction, by means of:

a.over-the-counter transactions;

b.mail order transactions;

c.telephone order transactions; and

2.is designed for installation by the user without further substantial support by the supplier.

3.  In this Group:

“3-D vector rate” means the number of vectors generated per second which have 10 pixel poly line vectors, clip tested, randomly oriented, with either integer or floating point X-Y-Z coordinate values, whichever produces the maximum rate;

“accuracy”, 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” means systems whose function is to prevent undesirable aircraft motions, rocket motions or structural loads by autonomously processing outputs from multiple sensors and then providing necessary preventive commands to effect automatic control;

“active pixel” means a minimum (single) element of the solid state array which has a photoelectric transfer function when exposed to light;

“adaptive control” means a control system that adjusts the response from conditions detected during the operation;

“angular position deviation” 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;

“ASTM” means the American Society for Testing and Materials;

“asynchronous transfer mode (ATM)” means a transfer mode in which the information is organised into cells; it is asynchronous in the sense that the recurrence of cells depends on the required or instantaneous bit rate;

“automatic target tracking” 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;

“bandwidth of one voice channel”, in the case of data communication equipment, means designed to operate in one voice channel of 3,100 Hz, as defined in CCITT Recommendation G.151;

“basic gate propagation delay time” means the propagation delay time value corresponding to the basic gate used within a family of monolithic integrated circuits; this may be specified, for a given family, either as the propagation delay time per typical gate or as the typical propagation delay time per gate;

“beat length” means the distance over which two orthogonally polarised signals, initially in phase, must pass in order to achieve a 2 Pi radian(s) phase difference;

“bias” means an accelerometer output when no acceleration is applied;

“camming” (axial displacement) 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;

“CCITT” means International Telegraph and Telephone Consultative Committee;

“CEP” (circle of equal probability) means a measure of accuracy defined as the radius of the circle centred at the target, at a specific range, in which 50% of the payloads impact;

“chemical laser” means a laser in which the excited species is produced by the output energy from a chemical reaction;

“circuit element” means a single active or passive functional part of an electronic circuit which may be a diode, a transistor, a resistor or a capacitor;

“circulation-controlled anti-torque or circulation-controlled directional control systems” means systems that use air blown over aerodynamic surfaces to increase or control the forces generated by the surfaces;

“commingled” means the filament to filament blending of thermoplastic fibres and reinforcement fibres in order to produce a fibre reinforcement matrix mix in total fibre form;

“comminution” means a process to reduce a material to particles by crushing or grinding;

“common channel signalling” means a signalling method in which a single channel between exchanges conveys, by means of labelled messages, signalling information relating to a multiplicity of circuits or calls and other information such as that used for network management;

“communications channel controller” 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;

“composite” 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;

“composite theoretical performance” (CTP) means a measure of computational performance given in millions of theoretical operations per second (Mtops), calculated using the aggregation of computing elements (CE);

Note to composite theoretical performance (CTP)

Abbreviations used in this Note
CEcomputing element (typically an arithmetic logical unit)
FPfloating point
XPfixed point
texecution time
XORexclusive OR
CPUcentral processing unit
TPtheoretical performance (of a single CE)
CTPcomposite theoretical performance (multiple CEs)
Mtopsmillions of theoretical operations per second
Reffective calculating rate
WLword length
Lword length adjustment
*multiply
Execution time 't' is expressed in microseconds, TP and CTP are expressed in millions of theoretical operations per second (Mtops) and WL is expressed in bits.

Outline of the CTP calculation method

The following table shows the method of calculating the effective calculating rate (R) for each CE:

Step 1: The effective calculating rate R

For CEs implementing Note: Every CE must be evaluated independentlyEffective calculating rate, R

XP only

(Rxp)

if no add is implemented use:

If neither add nor multiply is implemented use the fastest available arithmetic operation as follows:

See Notes X & Y

FP only

(Rfp)

Max

See Notes X & Z

Both FP and XP

(R)

Calculate both Rxp, Rfp
For simple logic processors not implementing any of the specified arithmetic operations.

Where

  • tlog is the execute time of the XOR, or for logic hardware not implementing the XOR, the fastest simple logic operation.

See Notes X & Z

For special logic processors not using any of the specified arithmetic or logic operations.

R = R'*WL / 64

Where

  • R' is the number of results per second, WL is the number of bits upon which the logic operation occurs, and 64 is a factor to normalize to a 64 bit operation.

Rates should be calculated for all supported operand lengths considering both pipelined operations (if supported), and non-pipelined operations using the fastest executing instruction for each operand length based on:

1. Pipelined or register-to-register operations. Exclude extraordinarily short execution times generated for operations on a predetermined operand or operands (for example, multiplication by 0 or 1). If no register-to-register operations are implemented, continue with (2).

2. The faster of register-to-memory or memory-to-register operations; if these also do not exist, then continue with (3).

3. Memory-to-memory.

In each case above, use the shortest execution time certified by the manufacturer.

Step 2:  TP for each supported operand length WL

Adjust the effective rate R (or R') by the word length adjustment L as follows:

Note: The word length WL used in these calculations is the operand length in bits. (If an operation uses operands of different lengths, select the largest word length.)

The combination of a mantissa ALU and an exponent ALU of a floating point processor or unit is considered to be one CE with a Word Length (WL) equal to the number of bits in the data representation (typically 32 or 64) for purposes of the CTP calculation.

This adjustment is not applied to specialized logic processors which do not use XOR instructions. In this case TP = R.

Select the maximum resulting value of TP for:

Step 3: CTP for aggregations of CEs, including CPUs

Category 1—Materials, Chemicals, Microorganisms & Toxins
Equipment, Assemblies and Components

1A—1A001 Components made from fluorinated compounds, as follows:

a.Seals, gaskets, sealants or fuel bladders specially designed for aircraft or aerospace use made from more than 50% of any of the materials specified in heads b. or c. of entry 1C009;

b.Piezoelectric polymers and copolymers made from vinylidene fluoride:

1.In sheet or film form; and

2.With a thickness exceeding 200 micrometre;

c.Seals, gaskets, valve seats, bladders or diaphragms made from fluoroelastomers containing at least one vinylether monomer, specially designed for aircraft, aerospace or missile use.

In this sub-head, “missile” means complete rocket systems and unmanned air vehicle systems.

1A002 Composite structures or laminates, as follows(1):

a.Having an organic matrix and made from materials specified in heads c., d. or e. of entry 1C010; or

b.Having a metal or carbon matrix and made from:

1.Carbon fibrous or filamentary materials with:

a.A specific modulus exceeding 10.15 × 106m; and

b.A specific tensile strength exceeding 17.7 × 104m; or

2.Materials specified in head c. of entry 1C010.

1A003 Manufactures of non-fluorinated polymeric substances specified in head a. of entry 1C008, in film, sheet, tape or ribbon form:

a.With a thickness exceeding 0.254 mm; or

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

1A102 Resaturated pyrolized carbon-carbon materials designed for systems specified in entries 9A004 or 9A104.

1A202 Composite structures, other than those specified in entry 1A002, in the form of tubes with an inside diameter of between 75 mm and 400 mm made with fibrous or filamentary materials specified in heads a. or b. of entry 1C010 or entry 1C210(2).

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 for use in separating heavy water from ordinary water and made of phosphor bronze mesh or copper (both chemically treated to improve wettability) and designed for use in vacuum distillation towers.

1A227 High-density (lead glass or other) radiation shielding windows greater than 0.3 m on a side and with a density greater than 3 g/cm3 and a thickness of 100 mm or greater and specially designed frames therefor.

1B  Test, Inspection and Production Equipment

1B001 Equipment for the production of fibres, prepregs, preforms or composites specified in entries 1A002 or 1C010, as follows, and specially designed components and accessories therefor(3):

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

b.Tape-laying or tow-placement machines of which the motions for positioning and laying tape, tows or sheets are coordinated and programmed in two or more axes, specially designed for the manufacture of composite airframe or missile structures;

c.Multidirectional, multidimensional weaving machines or interlacing machines, including adapters and modification kits, for weaving, interlacing or braiding fibres to manufacture composite structures;

d.Equipment specially designed or adapted for the production of reinforcement fibres, as follows:

1.Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, pitch or polycarbosilane) into carbon fibres or silicon carbide fibres, including special equipment to strain the fibre during heating;

2.Equipment for the chemical vapour deposition of elements or compounds on heated filamentary substrates to manufacture silicon carbide fibres;

3.Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide);

4.Equipment for converting aluminium containing precursor fibres into alumina fibres by heat treatment;

e.Equipment for producing prepregs specified in head e. of entry 1C010 by the hot melt method;

f.Non-destructive inspection equipment capable of inspecting defects three dimensionally, using ultrasonic or X-ray tomography and specially designed for composite materials.

In this entry, “missile” means complete rocket systems and unmanned air vehicle systems.

1B002 Systems and components therefor specially designed for producing metal alloys, metal alloy powder or alloyed materials specified in sub-head a.2. of entry 1C002, head b. of entry 1C002 or head c. of entry 1C002.

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

a.Airframe or aerospace structures;

b.Aircraft or aerospace engines; or

c.Specially designed components for those structures or engines.

1B101 Equipment, other than that specified in entry 1B001, for the production of structural composites as follows; and specially designed components and accessories therefor(4):

a.Filament winding machines of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and coordinating and programming controls;

b.Tape-laying machines of which the motions for positioning and laying tape and sheets can be coordinated and programmed in two or more axes, designed for the manufacture of composite airframe and missile structures;

c.Multi-directional, multi-dimensional weaving machines or interlacing machines, including adapters and modification kits for weaving, interlacing or braiding fibres to manufacture composite structures;

d.Equipment designed or modified for the production of fibrous or filamentary materials as follows:

1.Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon or polycarbosilane) including special provision to strain the fibre during heating;

2.Equipment for the vapour deposition of elements or compounds on heated filament substrates; and

3.Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide);

e.Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms specified in entry 9A110.

1B115 Equipment for the production, handling and acceptance testing of goods specified in entry 1C115, and specially designed components therefor.

a.Batch mixers having a total volumetric capacity of 110 litres or more and at least one mixing/kneading shaft mounted off centre;

b.Continuous mixers having two or more mixing/kneading shafts and capability to open the mixing chamber.

1B116 Specially designed nozzles for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1573 K (1300°C) to 3173 K (2900°C) temperature range at pressures of 130 Pa to 20 kPa.

1B201 Filament winding machines, other than those specified in entries 1B001 or 1B101, in which the motions for positioning, wrapping, and winding fibres are coordinated and programmed in two or more axes, specially designed to fabricate composite structures or laminates from fibrous or filamentary materials and capable of winding cylindrical rotors of diameter between 75 mm and 400 mm and lengths of 600 mm or greater and coordinating and programming controls and precision mandrels therefor.

1B225 Electrolytic cells for fluorine production with a production capacity greater than 250g 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.

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.

1B227 Ammonia synthesis converters, ammonia synthesis units in which the synthesis gas (nitrogen and hydrogen) is withdrawn from an ammonia/hydrogen high-pressure exchange column and the synthesized ammonia is returned to that column.

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

a.Designed to operate with internal temperatures of 35 K (-238°C) or less;

b.Designed to operate at an internal pressure of 0.5 to 5 MPa (5 to 50 atmospheres);

c.Constructed of fine-grain stainless steels of the 300 series with low sulphur content or equivalent cryogenic and H2-compatible materials; and

d.With internal diameters of 1 m or greater and effective lengths of 5 m or greater.

1B229 Water-hydrogen sulphide exchange tray columns constructed from fine carbon steel with a diameter of 1.8 m or greater to operate at a nominal pressure of 2 MPa or greater.

1.For columns which are specially designed or prepared for the production of heavy water see entry B40 of Group 2 of Part III of this Schedule.

2.This entry includes internal contactors of the columns, which are segmented trays with an effective assembled diameter of 1.8 m or greater, such as sieve trays, valve trays, bubble cap trays, and turbogrid trays designed to facilitate countercurrent contacting and constructed of materials resistant to corrosion by hydrogen sulphide/water mixtures, such as 304L or 316 stainless steel.

3.Fine Carbon steels include steels such as specified by ASTM A516.

1B230 Pumps circulating solutions of diluted or concentrated potassium amide catalyst in liquid ammonia (KNH2/NH3), with all of the following characteristics:

a.Airtight (i.e., hermetically sealed);

b.For concentrated potassium amide solutions (1% or greater), operating pressure of 1.5-60 MPa (15-600 atmospheres); for dilute potassium amide solutions (less than 1%), operating pressure of 20-60 MPa (200-600 atmospheres); and

c.A capacity greater than 8.5 m3/hr.

1B231 Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium, and equipment as follows:

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

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

1C  Materials

1C001 Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as follows(5):

a.Materials for absorbing frequencies exceeding 2 × 108 Hz but less than 3 × 1012 Hz; except:

b.Materials for absorbing frequencies exceeding 1.5 × 1014 Hz but less than 3.7 × 1014 Hz and not transparent to visible light;

c.Intrinsically conductive polymeric materials with a bulk electrical conductivity exceeding 10,000 S/m (Siemens per metre) or a sheet (surface) resistivity of less than 100 ohms/square, based on any of the following polymers:

1.Polyaniline;

2.Polypyrrole;

3.Polythiophene;

4.Poly phenylene-vinylene; or

5.Poly thienylene-vinylene.

1C002 Metal alloys, metal alloy powder or alloyed materials, as follows(6):

a.Metal alloys, as follows:

1.Nickel or titanium-based alloys in the form of aluminides, as follows, in crude or semi-fabricated forms:

a.Nickel aluminides containing 10 weight per cent or more aluminium;

b.Titanium aluminides containing 12 weight per cent or more aluminium;

2.Metal alloys, as follows, made from metal alloy powder or particulate material specified in head b. of this entry:

a.Nickel alloys with:

1.A stress-rupture life of 10,000 hours or longer at 923 K (650°C) at a stress of 550 MPa; or

2.A low cycle fatigue life of 10,000 cycles or more at 823 K (550°C) at a maximum stress of 700 MPa;

b.Niobium alloys with:

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

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

c.Titanium alloys with:

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

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

d.Aluminium alloys with a tensile strength of:

1.240 MPa or more at 473 K (200°C); or

2.415 MPa or more at 298 K (25°C);

e.Magnesium alloys with a tensile strength of 345 MPa or more and a corrosion rate of less than 1 mm/year in 3% sodium chloride aqueous solution measured in accordance with ASTM standard G-31;

Notes:

1.The metal alloys specified in head a. of this entry 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.

3.Low cycle fatigue life should be measured in accordance with ASTM Standard E-606 ‘Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing’. 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.

b.Metal alloy powder or particulate material for materials specified in head a. of this entry, as follows:

1.Made from any of the following composition systems:

a.Nickel alloys (Ni-Al-X, Ni-X-Al) qualified for turbine engine parts or components, i.e. with less than 3 non-metallic particles (introduced during the manufacturing process) larger than 100 micrometre in 109 alloy 15 particles;

b.Niobium alloys (Nb-Al-X or Nb-X-Al, Nb-Si-X or Nb-X-Si, Nb-Ti-X or Nb-X-Ti);

c.Titanium alloys (Ti-Al-X or Ti-X-Al);

d.Aluminium alloys (Al-Mg-X or Al-X-Mg, Al-Zn-X or Al-X-Zn, Al-Fe-X or Al-X-Fe); or

e.Magnesium alloys (Mg-Al-X or Mg-X-Al); and

2.Made in a controlled environment by any of the following processes:

a.Vacuum atomisation;

b.Gas atomisation;

c.Rotary atomisation;

d.Splat quenching;

e.Melt spinning and comminution;

f.Melt extraction and comminution; or

g.Mechanical alloying;

c.Alloyed materials, in the form of uncomminuted flakes, ribbons or thin rods produced in a controlled environment by splat quenching, melt spinning or melt extraction, used in the manufacture of metal alloy powder or particulate material specified in head b. of this entry.

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

a.Initial relative permeability of 120,000 or more and a thickness of 0.05 mm or less;

b.Magnetostrictive alloys with:

1.A saturation magnetostriction of more than 5 × 10−4 or

2.A magnetomechanical coupling factor (k) of more than 0.8; or

c.Amorphous alloy strips having both of the following characteristics:

1.A composition having a minimum of 75 weight percent of iron, cobalt or nickel; and

2.A saturation magnetic induction (Bs) of 1.6 T or more, and:

a.A strip thickness of 0.02 mm or less; or

b.An electrical resistivity of 2 × 10−4 ohm cm or more.

1C004 Uranium titanium alloys or tungsten alloys with a matrix based on iron, nickel or copper, with:

a.A density exceeding 17.5 g/cm3;

b.An elastic limit exceeding 1,250 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:

a.Multifilamentary superconductive composite conductors containing one or more niobium-titanium filaments:

1. Embedded in a matrix other than a copper or copper-based mixed matrix; or

2.With a cross-section area less than 0.28 × 10−4 mm2 (6 micrometre in diameter for circular filaments);

b.Superconductive composite conductors consisting of one or more superconductive filaments other than niobium-titanium:

1.With a critical temperature at zero magnetic induction exceeding 9.85 K (-263.31°C) but less than 24 K (-249.16°C);

2.With a cross-section area less than 0.28 × 10−4 mm2; and

3.Which remain in the superconductive state at a temperature of 4.2 K (-268.96°C) when exposed to a magnetic field corresponding to a magnetic induction of 12 T.

1C006 Fluids and lubricating materials, as follows:

a.Hydraulic fluids containing, as their principal ingredients, any of the following compounds or materials:

1.Synthetic hydrocarbon oils or silahydrocarbon oils with:

a.A flash point exceeding 477 K (204°C);

b.A pour point at 239 K (-34°C) or less;

c.A viscosity index of 75 or more; and

d.A thermal stability at 616 K (343°C); or

2.Chlorofluorocarbons with:

a.No flash point;

b.An autogenous ignition temperature exceeding 977 K (704°C);

c.A pour point at 219 K (-54°C) or less;

d.A viscosity index of 80 or more; and

e.A boiling point at 473 K (200°C) or higher;

b.Lubricating materials containing, as their principal ingredients, any of the following compounds or materials:

1.Phenylene or alkylphenylene ethers or thio-ethers, or their mixtures, containing more than two ether or thio-ether functions or mixtures thereof; or

2.Fluorinated silicone fluids with a kinematic viscosity of less than 5,000 mm2/s (5,000 centistokes) measured at 298 K (25°C);

c.Damping or flotation fluids with a purity exceeding 99.8%, containing less than 25 particles of 200 micrometre or larger in size per 100 ml and made from at least 85% of any of the following compounds or materials:

1.Dibromotetrafluoroethane;

2.Polychlorotrifluoroethylene (oily and waxy modifications only); or

3.Polybromotrifluoroethylene.

Notes:

1.Flash point is determined using the Cleveland Open Cup Methoddescribed in ASTM D-92.

2.Pour point is determined using the method described in ASTM D-97.

3.Viscosity index is determined using the method described in ASTM D-2270.

4.Thermal stability is determined by the following test procedure: 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 ± 6C) 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 methoddescribed in ASTM E-659.

1C007 Ceramic base materials, non-composite ceramic materials, ceramic-matrix composite materials and precursor materials, as follows(7):

a.Base materials 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 micrometre and no more than 10% of the particles larger than 10 micrometre;

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; except: Abrasives;

c.Ceramic-ceramic composite materials with a glass or oxide-matrix and reinforced with fibres from any of the following systems:

1.Si-N;

2.Si-C;

3.Si-Al-O-N; or

4.Si-O-N;

d.Ceramic-ceramic composite materials, with or without a continuous metallic phase, containing finely dispersed particles or phases of any fibrous or whisker-like material, where carbides or nitrides of silicon, zirconium or boron form the matrix;

e.Precursor materials (i.e., special purpose polymeric or metallo-organic materials) for producing any phase or phases of the materials specified in head c. of this entry, as follows:

1.Polydiorganosilanes (for producing silicon carbide);

2.Polysilazanes (for producing silicon nitride);

3.Polycarbosilazanes (for producing ceramics with silicon, carbon and nitrogen components).

1C008 Non-fluorinated polymeric substances, as follows:

a.1.Bismaleimides;

2.Aromatic polyamide-imides;

3.Aromatic polyimides;

4.Aromatic polyetherimides having a glass transition temperature (Tg) exceeding 503 K (230°C) as measured by the wet method;

b.Thermoplastic liquid crystal copolymers having a heat distortion temperature exceeding 523 K (250°C) measured according to ASTM D-648, method A, with a load of 1.82 N/mm2 and composed of:

1.Either of the following:

a.Phenylene, biphenylene or naphthalene; or

b.Methyl, tertiary-butyl or phenyl substituted phenylene, biphenylene or naphthalene; and

2.Any of the following acids:

a.Terephthalic acid;

b.6-hydroxy-2 naphthoic acid; or

c.4-hydroxybenzoic acid;

c.Polyarylene ether ketones, as follows:

1.Polyether ether ketone (PEEK);

2.Polyether ketone ketone (PEKK);

3.Polyether ketone (PEK);

4.Polyether ketone ether ketone ketone (PEKEKK);

d.Polyarylene ketones;

e.Polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof;

f.Polybiphenylenethersulphone.

1C009 Unprocessed fluorinated compounds, as follows:

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

b.Fluorinated polyimides containing 30% or more of combined fluorine;

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

1C010 Fibrous or filamentary materials which may be used in organic matrix, metallic matrix or carbon matrix composite structures or laminates, as follows(8):

a.Organic fibrous or filamentary materials (except polyethylene) with:

1.A specific modulus exceeding 12.7 × 106m; and

2.A specific tensile strength exceeding 23.5 × 104m;

b.Carbon fibrous or filamentary materials with:

1.A specific modulus exceeding 12.7 × 106m; and

2.A specific tensile strength exceeding 23.5 × 104m;

Notes:

1.Properties for materials described in this head should be determined using Suppliers of Advance Composite Materials Association (SACMA) recommended methods SRM 12 to 17 or Japanese Industrial Standard JIS-R-7601, Paragraph 6.6.2., and based on lot average.

2.This head does not specify fabric made from fibrous or filamentary materials for the repair of aircraft structures or laminates in which the size of individual sheets does not exceed 50 cm × 90 cm.

c.Inorganic fibrous or filamentary materials with:

1.A specific modulus exceeding 2.54 × 106m; and

2.A melting, decomposition or sublimation point exceeding 1,922 K (1,649°C) in an inert environment;

a.Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3 weight percent or more silica, with a specific modulus of less than 10 × 106m;

b.Molybdenum and molybdenum alloy fibres;

c.Boron fibres;

d.Discontinuous ceramic fibres with a melting, decomposition or sublimation point lower than 2,043 K (1,770°C) in an inert environment.

d.Fibrous or filamentary materials:

1.Composed of any of the following:

a.Polyetherimides specified in head a. of entry 1C008; or

b.Materials specified in heads b., c., d., e. or f. of entry 1C008; or

2.Composed of materials specified in sub-head d.1. of this entry and commingled with other fibres specified in heads a., b. or c. of this entry;

e.Resin- or pitch-impregnated fibres (prepregs), metal or carbon-coated fibres (preforms) or carbon fibre preforms, as follows:

1.Made from fibrous or filamentary materials specified in heads a., b. or c. of this entry;

2.Made from organic or carbon fibrous or filamentary materials:

a.With a specific tensile strength exceeding 17.7 × 104 m;

b.With a specific modulus exceeding 10.15 × 106m;

c.Not specified in heads a. or b. of this entry; and

d.When impregnated with materials specified in entry 1C008 or head b. of entry 1C009, or with phenolic or epoxy resins, having a glass transition temperature (Tg) exceeding 383 K (110°C).

1C101 Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), other than those specified in entry 1C001, usable in missiles and their subsystems.

1. Notes:

1.This entry 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, infra red or ultra violet regions of the electromagnetic spectrum.

2.This entry does not include coatings when specially used for the thermal control of satellites.

1C107 Graphite and ceramic materials, as follows:

a.Fine grain recrystallised bulk graphites, having a bulk density of 1.72 g/cm3 or greater, measured at 288 K (15°C), and having a particle size of 100 micrometres or less, pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips;

b.Ceramic composite materials (dielectric constant less than 6 at frequencies from 100 Hz to 10,000 MHz), usable for radomes, and bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips.

1C115 Propellants and constituent chemicals for propellants, as follows:

a.Propulsive substances:

1.Spherical aluminium powder, other than that specified in ML8 of Group 1 of Part III of this Schedule, with particles of uniform diameter of less than 500 micrometre and an aluminium content of 97% by weight or greater;

2.Metal fuels, other than that specified in ML8 of Group 1 of Part III of this Schedule, in particle sizes less than 500 micrometres, whether spherical, atomized, spheroidal, flaked or ground, consisting of 97% by weight or more of any of the following:

a.Zirconium;

b.Beryllium;

c.Boron;

d.Magnesium;

e.Zinc;

f.Alloys of the metals specified by a. to e. above; or

g.Misch metal;

3.Liquid oxidisers, the following:

a.Dinitrogen trioxide;

b.Nitrogen dioxide/dinitrogen tetroxide;

c.Dinitrogen pentoxide;

b.Polymeric substances:

1.Carboxy-terminated polybutadiene (CTPB);

2.Hydroxy-terminated polybutadiene (HTPB), other than that specified in ML8 of Group 1 of Part III of this Schedule;

3.Polybutadiene-acrylic acid (PBAA);

4.Polybutadiene-acrylic acid-acrylonitrile (PBAN);

c.Other propellant additives and agents:

1.Butacene;

2.Triethylene glycol dinitrate (TEGDN);

3.2-Nitrodiphenylamine.

1C116 Maraging steels (steels generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce age-hardening) having an ultimate tensile strength of 1500 MPa or greater, measured at 293 K (20°C), in the form of sheet, plate or tubing with a wall or plate thickness equal to or less than 5 mm(9).

1C117 Tungsten, molybdenum and alloys of these metals in the form of uniform spherical or atomized particles of 500 micrometre diameter or less with a purity of 97% or greater for fabrication of rocket motor components i.e. heat shields, nozzle substrates, nozzle throats and thrust vector control surfaces.

1C202 Alloys, other than those specified in sub-head a.2.c. or head d. of entry 1C002, as follows:

a.Aluminium alloys capable of an ultimate tensile strength of 460 MPa or more at 293 K (20°C), in the form of tubes or solid forms (including forgings) with an outside diameter of more than 75 mm;

b.Titanium alloys capable of an ultimate tensile strength of 900 MPa or more at 293 K (20°C) in the form of tubes or solid forms (including forgings) with an outside diameter of more than 75 mm.

In this entry, “alloys capable of” means alloys before or after heat treatment.

1C210 Fibrous or filamentary materials, other than those specified in heads a. or b. of entry 1C010, as follows:

a.Carbon or aramid fibrous or filamentary materials having a specific modulus of 12.7 × 106 m or greater or a specific tensile strength of 23.5 × 104 m or greater; or

b.Glass fibrous or filamentary materials having a specific modulus of 3.18 × 106 m or greater and a specific tensile strength of 7.62 × 104 m or greater.

1C216 Maraging steel, other than that specified in entry 1C116, capable of an ultimate tensile strength of 2,050 MPa or more, at 293 K (20°C);

1C225 Boron and boron compounds, mixtures and loaded materials in which the boron-10 isotope is more than 20% by weight of the total boron content.

1C226 Tungsten, as follows: parts made of tungsten, tungsten carbide, or tungsten alloys (greater than 90% tungsten) having a mass greater than 20 kg and a hollow cylindrical symmetry (including cylinder segments) with an inside diameter greater than 100 mm but less than 300 mm;

1C227 Calcium (high purity) containing both less than 1,000 parts per million by weight of metallic impurities other than magnesium and less than 10 parts per million of boron.

1C228 Magnesium (high purity) containing both less than 200 parts per million by weight of metallic impurities other than calcium and less than 10 parts per million of boron.

1C229 High purity (99.99% or greater) bismuth with very low silver content (less than 10 parts per million).

1C230 Beryllium metal, alloys containing more than 50% of beryllium by weight, compounds containing beryllium, and manufactures thereof; except:

a.Metal Windows for X-ray machines;

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

1C231 Hafnium metal, alloys and compounds of hafnium containing more than 60% hafnium by weight and manufactures thereof.

1C232 Helium in any form isotopically enriched in the helium-3 isotope, whether or not mixed with any other materials or contained in any equipment or device;except:

1C233 Lithium, as follows:

a.Metal, hydrides or alloys containing lithium enriched in the 6 isotope (6Li) to a concentration higher than the one existing in nature (7.5 % weight percent);

b.Any other materials containing lithium enriched in the 6 isotope (including compounds, mixtures and concentrates);

1C234 Zirconium as follows: metal, alloys containing more than 50% zirconium by weight, and compounds in which the ratio of hafnium content to zirconium content is less than 1 part to 500 parts by weight, and manufactures wholly thereof;

1C235 Tritium, tritium compounds, and mixtures containing tritium in which the ratio of tritium to hydrogen by atoms exceeds 1 part in 1000;

1C236 Alpha-emitting radionuclides having an alpha half-life of 10 days or greater but less than 200 years, including equipment, compounds and mixtures containing these radionuclides with a total alpha activity of 1 curie per kilogram (37 GBq/kg) or greater;

1C237 Radium-226;

1C238 Chlorine trifluoride (ClF3).

1C239 High explosives(10), other than those specified in ML8 of Group 1 of Part III of this Schedule, or substances or mixtures containing more than 2% thereof, with a crystal density greater than 1.8 gm/cm3 and having a detonation velocity greater than 8,000 m/s.

1C350 Chemicals, which may be used as precursors for toxic chemical agents, as follows, and preparations thereof(11):

a.1.Ammonium hydrogen fluoride;

2.Arsenic trichloride;

3.Benzilic acid;

4.2-Chloroethanol;

5.Diethylaminoethanol;

6.Diethyl ethylphosphonate;

7.Diethyl methylphosphonite;

8.Diethyl-N,N-dimethylphosphoramidate;

9.Diethyl phosphite;

10.Diisopropylamine;

11.N,N-Diisopropyl-(beta)-aminoethane thiol;

12.N,N-Diisopropyl-(beta)-amino ethanol;

13.N,N-Diisopropyl-(beta)-aminoethyl chloride;

14.N,N-Diisopropyl-(beta)-aminoethyl chloride hydrochloride;

15.Dimethyl ethylphosphonate;

16.Dimethyl methylphosphonate;

17.Dimethyl phosphite;

18.Dimethylamine;

19.Dimethylamine hydrochloride;

20.Ethyl phosphinyl dichloride;

21.Ethyl phosphinyl difluoride;

22.Ethyl phosphonyl dichloride;

23.Ethyl phosphonyl difluoride;

24.Hydrogen fluoride;

25.3-Hydroxy-1-methylpiperidine;

26.Methyl benzilate;

27.Methyl phosphinyl dichloride;

28.Methyl phosphinyl difluoride;

29.Methyl phosphonyl dichloride;

30.Phosphorus oxychloride;

31.Phosphorus pentachloride;

32.Phosphorus pentasulphide;

33.Phosphorus trichloride;

34.Pinacolone;

35.Pinacolyl alcohol;

36.Potassium fluoride;

37.Potassium cyanide;

38.Potassium hydrogen fluoride;

39.3-Quinuclidinol;

40.3-Quinuclidone;

41.Sodium bifluoride;

42.Sodium cyanide;

43.Sodium fluoride;

44.Sodium sulphide;

45.Sulphur dichloride;

46.Sulphur monochloride;

47.Thiodiglycol;

48.Thionyl chloride;

49.Triethanolamine;

50.Triethanolamine hydrochloride;

51.Triethyl phosphite;

52.Trimethyl phosphite;

1C351 Human pathogens, zoonoses and toxins (12):

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.Chikungunya virus;

2.Congo-Crimean haemorrhagic fever virus;

3.Dengue fever virus;

4.Eastern equine encephalitis virus;

5.Ebola virus;

6.Hantaan virus;

7.Junin virus;

8.Lassa fever virus;

9.Lymphocytic choriomeningitis virus;

10.Machupo virus;

11.Marburg virus;

12.Monkey pox virus;

13.Rift Valley fever virus;

14.Russian Spring-Summer encephalitis virus;

15.Variola virus;

16.Venezuelan equine encephalitis virus;

17.Western equine encephalitis virus;

18.White pox;

19.Yellow fever virus;

20.Japanese encephalitis virus;

b.Rickettsiae, 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.Coxiella burnetii;

2.Rickettsia quintana;

3.Rickettsia prowasecki;

4.Rickettsia rickettsii;

c.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:

1.Bacillus anthracis;

2.Brucella abortus;

3.Brucella melitensis;

4.Brucella suis;

5.Chlamydia psittaci;

6.Clostridium botulinum;

7.Francisella tularensis;

8.Pseudomonas mallei (Burkholderia mallei);

9.Pseudomonas pseudomallei (Burkholderia pseudomallei;

10.Salmonella typhi;

11.Shigella dysenteriae;

12.Vibrio cholerae;

13.Pasteurella pseudotuberculosis var pestis (Yersinia pestis);

d.Toxins, as follows;

1.Botulinum toxins;

2.Clostridium perfringens toxins;

3.Conotoxin;

4.Ricin;

5.Saxitoxin;

6.Shiga toxin;

7.Staphylococcus aureus toxins;

8.Tetrodotoxin;

9.Verotoxin;

10.Microcystins (Cyanginosins);

1C352 Animal Pathogens, as follows(14):

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 swine fever virus;

2.Avian influenza virus, which are:

a.Uncharacterised; or

b.Those defined in Council Directive 92/40/EEC(15), as having high pathogenicity, as follows:

1.Type A viruses with an IVPI (intravenous pathogenicity index) in 6 week old chickens of greater than 1.2; or

2.Type A viruses H5 or H7 subtype for which nucletide sequencing has demonstrated multiple basic amino acids at the cleavage site of haemagglutinin;

3.Bluetongue virus;

4.Foot and mouth disease virus;

5.Goat pox virus;

6.Porcine herpes virus (Aujeszky’s disease);

7.Swine fever virus (Hog cholera virus);

8.Lyssa virus;

9.Newcastle disease virus;

10.Peste des petits ruminants virus;

11.Swine vesicular disease (porcine enterovirus type 9);

12.Rinderpest virus;

13.Sheep pox virus;

14.Teschen disease virus;

15.Vesicular stomatitis virus;

b.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 Mycoplasma mycoides;

1C353 Genetically-modified microorganisms, as follows(16):

a.Genetically modified microorganisms or genetic elements that contain nucleic acid sequences associated with pathogenicity and are derived from organisms specified in heads a. to c. of entry 1C351 or entries 1C352 or 1C354;

b.Genetically modified microorganisms or genetic elements that contain nucleic acid sequences coding for any of the toxins specified in head d. of entry 1C351.

1C354 Plant pathogens, as follows:

a.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 campestris pv. citri including strains referred to as Xanthomonas campestris pv. citri types A,B,C,D,E or otherwise classified as Xanthomonas citri, Xanthomonas campestris pv. aurantifolia or Xanthomonas campestris pv. citrumelo;

b.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 coffeanum var. virulans;

2.Cochlibolus miyabeanus (Helminthosporium oryzae);

3.Microcyclus ulei(syn. Dothidella ulei);

4.Puccinia graminis (syn. Puccinia graminis f. sp. tritici);

5.Puccinia striiformis (syn. Puccinia glumarum);

6.Magnaporthe grisea (Pyricularia grisea/Pyricularia oryzae).

1C991 Other explosives and propellants and related substances as follows(17):

a.Amatol;

b.Nitrocellulose (containing more than 12.5% nitrogen);

c.Nitroglycol;

d.Pentaerythritol tetranitrate (PETN);

e.Picryl chloride;

f.Trinitrophenylmethylnitramine (tetryl);

g.2,4,6-Trinitrotoluene (TNT).

1C992 Vaccines for protection against either of the following:

a.Bacillus anthracis; or

b.Botulinum toxin.

1D  Software

1D001 Software specially designed or modified for the development, production or use of goods specified in entries 1B001 to 1B003.

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

1D101 Software specially designed for the use of goods specified in entry 1B101.

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 entry 1B201.

1E  Technology

1E001 Technology required for the development or production of goods specified in heads b. or c. of entry 1A001, or entries 1A002, 1A003, or sub-categories 1B or 1C.

1E002 Other technology:

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 base materials or non-composite ceramic materials:

1.Base materials having all of the following characteristics:

a.Any of the following compositions:

1.Single or complex oxides of zirconium and complex oxides of silicon or aluminium;

2.Single nitrides of boron (cubic crystalline forms);

3.Single or complex carbides of silicon or boron; or

4.Single or complex nitrides of silicon;

b.Total metallic impurities, excluding intentional additions, of less than:

1.1,000 ppm for single oxides or carbides; or

2.5,000 ppm for complex compounds or single nitrides; and

1.

Average particle size equal to or less than 5 micrometre and no more than 10% of the particles larger than 10 micrometre; or

Note: For zirconia, these limits are 1 micrometre and 5 micrometre respectively.

2.
a.

Platelets with a length to thickness ratio exceeding 5;

b.

Whiskers with a length to diameter ratio exceeding 10 for diameters less than 2 micrometre; and

c.

Continuous or chopped fibres less than 10 micrometre in diameter;

2.Non-composite ceramic materials (except abrasives) composed of the materials described in sub-head c.1. of this entry;

d.Technology for the production of aromatic polyamide fibres;

e.Technology for the installation, maintenance or repair of materials specified in entry 1C001;

f.Technology for the repair of composite structures, laminates or materials specified in entry 1A002 and heads c. or d. of entry 1C007.

1E101 Technology required for the use of goods specified in entries 1A102, 1B001, 1B101, 1B115, 1B116, 1C001, 1C101, 1C107, 1C115 to 1C117, 1D101 or 1D103.

1E102 Technology required for the development of software specified in entries 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 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.Note: This entry includes technology for the composition of precursor gases, flowrates and process control schedules and parameters.

1E201 Technology required for the use of goods specified in entries 1A002, 1A202, 1A225 to 1A227, 1B201, 1B225 to 1B231, sub-heads a.2.c. and a.2.d. of entry 1C002, head b. of entry 1C010, or entries 1C202, 1C210, 1C216, 1C225 to 1C239 or 1D201.

1E202 Technology required for the development or production of goods specified in entries 1A202, 1A225 to 1A227.

1E203 Technology required for the development of software specified in entry 1D201.

Category 2—Materials Processing
Equipment, Assemblies and Components

2A  Notes to 2A001 to 2A006:

1. DN is the product of the bearing bore diameter in mm and the bearing rotational velocity in rpm.

2. Operating temperatures include those temperatures obtained when a gas turbine engine has stopped after operation.

2A001 Ball bearings or solid roller bearings (except tapered roller bearings) having tolerances specified by the manufacturer in accordance with ISO Standard Class 4 (Annular Bearing Engineers Committee (ABEC) 7, ABEC 7P, ABEC 7T) or better, and having any of the following characteristics:

a.Rings, balls or rollers made from monel or beryllium;

b.Manufactured for use at operating temperatures above 573 K (300°C) either by using special materials or by special heat treatment; or

c.With lubricating elements or component modifications that, according to the manufacturer’s specifications, are specially designed to enable the bearings to operate at speeds exceeding 2.3 million DN.

2A002 Other ball bearings or solid roller bearings (except tapered roller bearings) having tolerances specified by the manufacturer in accordance with ISO Standard Class 2 (Annular Bearing Engineers Committee (ABEC) 9, ABEC 9P or better).

2A003 Solid tapered roller bearings, having tolerances specified by the manufacturer in accordance with American National Standards Institute (ANSI)/Anti-Friction Bearing Manufacturers Association (AFBMA) Class 00 (inch) or Class A (metric) or better and having either of the following characteristics:

a.With lubricating elements or component modifications that, according to the manufacturer’s specifications, are specially designed to enable the bearings to operate at speeds exceeding 2.3 million DN; or

b.Manufactured for use at operating temperatures below 219 K (-54°C) or above 423 K (150°C).

2A004 Gas-lubricated foil bearings manufactured for use at operating temperatures of 561 K (288°C) or higher and with a unit load capacity exceeding 1 MPa.

2A005 Active magnetic bearing systems.

2A006 Fabric-lined self-aligning or fabric-lined journal sliding bearings manufactured for use at operating temperatures below 219 K (-54°C) or above 423 K (150°C).

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

a.Crucibles with a volume of between 150 ml and 8 litres and made of or coated with any of the following materials having a purity of 98% or greater:

1.Calcium fluoride (CaF2);

2.Calcium zirconate (metazirconate) (Ca2ZrO3);

3.Cerium sulphide (Ce2S3);

4.Erbium oxide (erbia) (Er203);

5.Hafnium oxide (hafnia) (HfO2);

6.Magnesium oxide (MgO);

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

8.Yttrium oxide (yttria) (Y2O3); or

9.Zirconium oxide (zirconia) (ZrO2);

b.Crucibles with a volume of between 50 ml and 2 litres and made of or lined with tantalum, having a purity of 99.9% or greater;

c.Crucibles with a volume of between 50 ml and 2 litres and made of or lined with tantalum (having a purity of 98% or greater) coated with tantalum carbide, nitride or boride (or any combination of these).

2A226 Valves 5 mm or greater in diameter, with a bellows seal, wholly made of or lined with aluminium, aluminium alloy, nickel or alloy containing 60% or more nickel, either manually or automatically operated.

2B Test, Inspection and Production Equipment

2B001 Numerical control units, motion control boards specially designed for numerical control applications on machine tools, machine tools, and specially designed components therefor, as follows:

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.

2.Axis nomenclature shall be in accordance with International Standard ISO 841, ‘Numerical Control Machines – Axis and Motion Nomenclature’.

a.Numerical control units for machine tools, as follows, and specially designed components therefor:

a.Modified for and incorporated in machines not specified in this entry; or

b.Specially designed for machines not specified in this entry.

1.Having more than four interpolating axes which can be coordinated simultaneously for contouring control;

2.Having two, three or four interpolating axes which can be coordinated simultaneously for contouring control and:

a.Capable of real time processing of data to modify, during the machining operation, tool path, feed rate and spindle data by either:

1.Automatic calculation and modification of part programme data for machining in two or more axes by means of measuring cycles and access to source data; or

2.Adaptive control with more than one physical variable measured and processing by means of a computing model (strategy) to change one or more machining instructions to optimize the process;

b.Capable of receiving directly (on-line) and processing computer aided design (CAD) data for internal preparation of machine instructions; or

c.Capable, without modification, according to the manufacturer’s technical specifications, of accepting additional boards which would permit an increase above the levels specified in this entry, in the number of interpolating axes which can be coordinated simultaneously for contouring control, even if they do not contain these additional boards;

b.Motion control boards specially designed for machine tools and having any of the following characteristics:

1.Interpolation in more than four axes;

2.Capable of real time processing as described in sub-head a.2.a. of this entry; or

3.Capable of receiving and processing CAD data as described in sub-head a.2.b. of this entry;

c.Machine tools, as follows, for removing or cutting metals, ceramics or composites, which, according to the manufacturer’s technical specifications, can be equipped with electronic devices for simultaneous contouring control in two or more axes:

1.Machine tools for turning, grinding, milling or any combination thereof which:

a.Have two or more axes which can be coordinated simultaneously for contouring control; and

b.Have any of the following characteristics:

1.Two or more contouring rotary axes;

2.One or more contouring tilting spindles;

3.Camming (axial displacement) in one revolution of the spindle less (better) than 0.0006 mm total indicator reading (TIR);

4.Run out (out-of-true running) in one revolution of the spindle less (better) than 0.0006 mm TIR;

5.The positioning accuracies, with all compensations available, are less (better) than:

a.0.001° on any rotary axis; or

b.

1.0.004 mm along any linear axis (overall positioning) for grinding machines;

2.0.006 mm along any linear axis (overall positioning) for turning or milling machines; or

Notes:

1.Sub-head c.1.b.5. of this entry does not specify milling or turning machine tools with a positioning accuracy along one axis, with all compensations available, equal to or more (worse) than 0.005 mm.

2.The positioning accuracy of numerically controlled machine tools is to be determined and presented in accordance with ISO 230/2 paragraph 2.13, in conjunction with the requirements below:

a.Test conditions (paragraph 3):

1.For 12 hours before and during measurements, the machine tool and accuracy measuring equipment will be kept at the same ambient temperature. During the premeasurement time the slides of the machine will be continuously cycled in the same manner that the accuracy measurements will be taken;

2.The machine shall be equipped with any mechanical, electronic, or software compensation to be exported with the machine;

3.Accuracy of measuring equipment for the measurements shall be at least four times more accurate than the expected machine tool accuracy;

4.Power supply for slide drives shall be as follows:

a.Line voltage variation shall not exceed ± 10% of nominal rated voltage;

b.Frequency variation shall not exceed ±2 Hz of normal frequency;

c.Lineouts or interrupted service are not permitted;

b.Test programme (paragraph 4):

1.Feed rate (velocity of slides) during measurement shall be the rapid traverse rate, except in the case of machine tools which generate optical quality surfaces, the feed rate shall be equal to or less than 50 mm per minute;

2.Measurements shall be made in an incremental manner from one limit of the axis travel to the other without returning to the starting position for each move to the target position;

3.Axes not being measured shall be retained at mid travel during test of an axis;

c.Presentation of test results (paragraph 2): The results of the measurements must include:

1.Positioning accuracy (A); and

2.The mean reversal error (B).

6.

a.A positioning accuracy less (better) than 0.007 mm; and

b.A slide motion from rest for all slides within 20% of a motion command input for inputs of less than 0.5 micrometre;

Notes:

1.Minimum increment of motion test (slide motion from rest): The test is conducted only if the machine tool is equipped with a control unit the minimum increment of which is less (better) than 0.5 micrometre. Prepare the machine for testing in accordance with ISO 230/2 paragraphs 3.1, 3.2, 3.3.Conduct the test on each axis (slide) of the machine tool as follows:

a.Move the axis over at least 50% of the maximum travel in plus and minus directions twice at maximum feed rate, rapid traverse rate or jog control;

b.Wait at least 10 seconds;

c.With manual data input, input the minimum programmable increment of the control unit;

d.Measure the axis movement;

e.Clear the control unit with the servo null, reset or whatever clears any signal (voltage) in the servo loop;

f.Repeat steps b. to e. above five times, twice in the same direction of the axis travel and three times in the opposite direction of travel for a total of six test points;

g.If the axis movement is between 80% and 120% of the minimum programmable input for four of the six test points, the machine is controlled.

2.Sub-head c.1. of this entry does not specify cylindrical external, internal and external-internal grinding machines having all of the following characteristics:

a.Not centreless (shoe-type) grinding machines;

b.Limited to cylindrical grinding;

c.A maximum workpiece capacity of 150 mm outside diameter or length;

d.Only two axes which can be coordinated simultaneously for contouring control; and

e.No contouring c axis.

3.Sub-head c.1. of this entry does not specify machines designed specifically as jig grinders having both of the following characteristics:

a.Axes limited to x, y, c and a, where the c axis is used to maintain the grinding wheel normal to the work surface and the a axis is configured to grind barrel cams; and

b.A spindle run out not less (not better) than 0.0006 mm.

4.Sub-head c.1. of this entry does not specify tool or cutter grinding machines having all of the following characteristics:

a.Shipped as a complete system with software specially designed for the production of tools or cutters;

b.No more than two rotary axes which can be coordinated simultaneously for contouring control;

c.Run out (out-of-true running) in one revolution of the spindle not less (not better) than 0.0006 mm TIR; and

d.The positioning accuracies, with all compensations available, are not less (not better) than:

1.0.004 mm along any linear axis for overall positioning; or

2.0.001° on any rotary axis.

2.Electrical discharge machines (EDM) of the wire feed type which have five or more axes which can be coordinated simultaneously for contouring control;

3.Electrical discharge machines (EDM) of the non-wire type which have two or more rotary axes which can be coordinated simultaneously for contouring control;

4.Machine tools for removing metals, ceramics or composites:

a.By means of:

1.Water or other liquid jets, including those employing abrasive additives;

2.Electron beam; or

3.Laser beam; and

b.Having two or more rotary axes which:

1.Can be coordinated simultaneously for contouring control; and

2.Have a positioning accuracy of less (better) than 0.003°.

2B002 Non-numerically controlled machine tools for generating optical quality surfaces, as follows:

a.Turning machines using a single point cutting tool and having all of the following characteristics:

1.Slide positioning accuracy less (better) than 0.0005 mm per 300 mm of travel;

2.Bidirectional slide positioning repeatability less (better) than 0.00025 mm per 300 mm of travel;

3.Spindle run out and camming less (better) than 0.0004 mm TIR;

4.Angular deviation of the slide movement (yaw, pitch and roll) less (better) than 2 seconds of arc, TIR, over full travel; and

5.Slide perpendicularity less (better) than 0.001 mm per 300 mm of travel;

b.Fly cutting machines having both of the following characteristics:

1.Spindle run out and camming less (better) than 0.0004 mm TIR; and

2.Angular deviation of slide movement (yaw, pitch and roll) less (better) than 2 seconds of arc, TIR, over full travel.

2B003 Numerically controlled or manual machine tools specially designed for cutting, finishing, grinding or honing either of the following classes of bevel or parallel axis hardened (Rc = 40 or more) gears, and specially designed components, controls and accessories therefor:

a.Hardened bevel gears finished to a quality of better than ISO 1328 class 4; or

b.Hardened 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 ISO 1328 class 3 or better.

2B004 Hot isostatic presses, as follows, and specially designed dies, moulds, components, accessories and controls therefor(18):

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

b.Having:

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.

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 head d. of entry 2E003, and specially designed automated handling, positioning, manipulation and control components therefor:

a.Stored programme controlled chemical vapour deposition (CVD) production equipment with both of the following:

1.Process modified for one of the following:

a.Pulsating CVD;

b.Controlled nucleation thermal decomposition (CNTD); or

c.Plasma enhanced or plasma assisted CVD; and

2.Either of the following:

a.Incorporating high vacuum (equal to or less than 0.01 Pa) rotating seals; or

b.Incorporating in situ coating thickness control;

b.Stored programme controlled ion implantation production equipment having beam currents of 5 mA or more;

c.Stored programme controlled electron beam physical vapour deposition (EBPVD) production equipment incorporating:

1.Power systems rated for over 80 kW;

2.A liquid pool level laser control system which regulates precisely the ingots feed rate; and

3.A computer controlled rate monitor operating on the principle of photoluminescence of the ionised atoms in the evaporant stream to control the deposition rate of a coating containing two or more elements;

d.Stored programme controlled plasma spraying production equipment having either of the following characteristics:

1.Operating at reduced pressure controlled atmosphere (equal to or less than 10 kPa measured above and within 300 mm of the gun nozzle exit) in a vacuum chamber capable of evacuation down to 0.01 Pa prior to the spraying process; or

2.Incorporating in situ coating thickness control;

e.Stored programme controlled sputter deposition production equipment capable of current densities of 0.1 mA/mm2 or higher at a deposition rate of 15 micrometre/hr or more;

f.Stored programme controlled cathodic arc deposition production equipment incorporating a grid of electromagnets for steering control of the arc spot on the cathode;

g.Stored programme controlled ion plating production equipment allowing for the in situ measurement of either:

1.Coating thickness on the substrate and rate control; or

2.Optical characteristics.

2B006 Dimensional inspection or measuring systems or equipment, as follows:

a.Computer controlled, numerically controlled or stored programme controlled dimensional inspection machines, having both of the following characteristics:

1.Two or more axes; and

2.A one dimensional length measurement uncertainty equal to or less (better) than (1.25 + L/1,000) micrometre tested with a probe with an accuracy of less (better) than 0.2 micrometre (L is the measured length in mm);

b.Linear and angular displacement measuring instruments, as follows:

1.Linear measuring instruments having any of the following characteristics:

a.Non-contact type measuring systems with a resolution equal to or less (better) than 0.2 micrometre within a measuring range up to 0.2 mm;

b.Linear voltage differential transformer systems with both of the following characteristics:

1.Linearity equal to or less (better) than 0.1% within a measuring range up to 5 mm; and

2.Drift equal to or less (better) than 0.1% per day at a standard ambient test room temperature ±1 K; or

c.Measuring systems having both of the following characteristics:

1.Containing a laser; and

2.Maintaining, for at least 12 hours, over a temperature range of ± 1 K around a standard temperature and at a standard pressure:

a.A resolution over their full scale of 0.1 micrometre or less (better); and

b.A measurement uncertainty equal to or less (better) than (0.2 +L/2,000) micrometre (L is the measured length in mm);

2.Angular measuring instruments having an angular position deviation equal to or less (better) than 0.00025°;

c.Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics:

1.Measurement uncertainty along any linear axis equal to or less (better) than 3.5 micrometre per 5 mm; and

2.Angular position deviation equal to or less (better) than 0.02°;

d.Equipment for measuring surface irregularities, by measuring optical scatter as a function of angle, with a sensitivity of 0.5 nm or less (better).

Notes:

1.The probe used in determining the measurement uncertainty of a dimensional inspection system shall be as described in Verein Deutscher Ingenieure (VDI) / Verband Deutscher Elektrotechniker (VDE) 2617 Parts 2, 3 and 4.

2.All measurement values in this entry represent permissible positive and negative deviations from the target value, i.e., not total band.

3.Machine tools which can be used as measuring machines are specified if they meet or exceed the criteria specified for the machine tool function or the measuring machine function.

4.A machine described in this entry is specified if it exceeds the threshold anywhere within its operating range.

5.In this entry measurement uncertainty means 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 (Reference: VDI/VDE 2617).

2B007 Robots, as follows, and specially designed controllers and end-effectors therefor(19):

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;

b.Specially designed to comply with national safety standards applicable to explosive munitions environments; or

c.Specially designed or rated as radiation-hardened beyond that necessary to withstand normal industrial (i.e., non-nuclear industry) ionizing radiation.

2B008 Assemblies, units or inserts specially designed for machine tools, or for equipment specified in entries 2B006 or 2B007, as follows:

a.Spindle assemblies, consisting of spindles and bearings as a minimal assembly, with radial (run out) or axial (camming) axis motion in one revolution of the spindle less (better) than 0.0006 mm TIR;

b.Linear position feedback units (e.g., inductive type devices, graduated scales, infrared systems or laser systems) having an overall accuracy less (better) than (800 + (600 × L × 10−3)) nm (L equals the effective length in mm);

c.Rotary position feedback units, e.g., inductive type devices, graduated scales, infrared systems or laser systems, having an accuracy less (better) than 0.00025°;

d.Slide way assemblies consisting of a minimal assembly of ways, bed and slide having all of the following characteristics:

1.A yaw, pitch or roll of less (better) than 2 seconds of arc TIR over full travel;

2.A horizontal straightness of less (better) than 2 micrometre per 300 mm length; and

3.A vertical straightness of less (better) than 2 micrometre per 300 mm length;

e.Single point diamond cutting tool inserts, having all of the following characteristics:

1.Flawless and chip-free cutting edge when magnified 400 times in any direction;

2.Cutting radius from 0.1 to 5 mm inclusive; and

3.Cutting radius out-of-roundness less (better) than 0.002 mm TIR.

2B009 Specially designed printed circuit boards with mounted components and software therefor, or compound rotary tables or tilting spindles, capable of upgrading, according to the manufacturer’s specifications, numerical control units, machine tools or feed-back devices to or above the levels specified in entries 2B001 to 2B008.

2B104 Equipment and process controls designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips.

2B115 Flow-forming machines, and specially designed components therefor(20), which:

a.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

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

2B116 Vibration test equipment and components therefor, the following:

a.Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at 10 g rms or more over the entire range 20 Hz to 2000 Hz and imparting forces of 50 kN (11,250 lbs), measured bare table, or greater;

b.Digital controllers, combined with specially designed vibration test software, with a real-time bandwidth greater than 5 kHz and designed for use with vibration test systems in head a. of this entry;

c.Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force of 50 kN (11,250 lbs), measured bare table, or greater and usable in vibration test systems in head a. of this entry;

d.Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force of 50 kN, measured bare table, or greater, and usable in vibration systems in head a. of this entry.

In this entry, “bare table” means a flat table, or surface, with no fixtures or fittings.

2B204 Isostatic presses, other than those specified in entries 2B004 or 2B104, capable of achieving a maximum working pressure of 69 MPa or greater and having a chamber cavity with an inside diameter in excess of 152 mm and specially designed dies, moulds and controls therefor.

2B207 Robots and end-effectors, other than those specified in entry 2B007, specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives) and specially designed controllers therefor.

2B215 Spin-forming and flow-forming machines, other than those specified in entry 2B115, and precision rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm therefor, which:

a.According to the manufacturer’s technical specification, can be equipped with numerical control units or a computer control; and

b. With two or more axes that can be coordinated simultaneously for contouring control.

2B225 Remote manipulators that provide mechanical translation of human operator actions by electrical, hydraulic or mechanical means to an operating arm and terminal fixture that can be used to provide remote actions in radiochemical separation operations and hot cells, as follows:

a.Having a capability of penetrating 0.6 m or more of cell wall; or

b.Having a capability to bridge over the top of a cell wall with a thickness of 0.6 m or more.

2B226 Vacuum or controlled environment (inert gas) induction furnaces capable of operating above 1,123 K (850°C) and having induction coils 600 mm or less in diameter and specially designed power supplies therefor with an output rating of 5 kW or more(21).

2B227 Vacuum and controlled atmosphere metallurgical melting and casting furnaces as follows; and specially configured computer control and monitoring systems therefor:

a.Arc remelt and casting furnaces with consumable electrode capacities between 1000 cm3 and 20,000 cm3, capable of operating with melting temperatures above 1973 K (1700°C);

b.Electron beam melting and plasma atomization and melting furnaces, with a power of 50 kW or greater, capable of operating with melting temperatures above 1473 K (1200°C).

2B228 Rotor fabrication and assembly equipment and bellows-forming mandrels and dies, as follows:

a.Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles and end caps, including associated precision mandrels, clamps and shrink fit machines;

b.Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;

c.Bellows-forming mandrels and dies for producing single-convolution bellows (bellows made of high-strength aluminium alloys, maraging steel or high strength filamentary materials). The bellows have all of the following dimensions:

1.75 mm to 400 mm inside diameter;

2.12.7 mm or more in length; and

3.Single convolution depth more than 2 mm.

2B229 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.A swing or journal diameter of 75 mm or more;

2.Mass capability of from 0.9 to 23 kg; and

3.Capable of balancing speed of revolution more than 5000 rpm;

b.Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:

1.A journal diameter of 75 mm or more;

2.Mass capability of from 0.9 to 23 kg;

3.Capable of balancing to a residual imbalance of 0.01 kg mm/kg per plane or better; and

4.Belt drive type.

2B230 Instruments capable of measuring pressures up to 13 kPa to an accuracy of better than 1% (full-scale), with corrosion-resistant pressure-sensing elements constructed of nickel, nickel alloys, phosphor bronze, stainless steel, aluminium or aluminium alloys.

2B231 Vacuum pumps with an input throat size of 380 mm or greater with a pumping speed of 15,000 litres/s or greater and capable of producing an ultimate vacuum better than 13 mPa.

2B232 Multistage light gas gun or other high-velocity gun systems (coil, electromagnetic, electrothermal or other advanced systems) capable of accelerating projectiles to 2 km/s or greater.

2B350 Chemical manufacturing facilities and equipment, 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;

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; or

7.Zirconium or zirconium alloys;

b.Agitators for use in reaction vessels or reactors 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;

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; or

7.Zirconium or zirconium 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;

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; or

7.Zirconium or zirconium alloys;

d.Heat exchangers or condensers with a heat transfer surface area of less than 20 m2, 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;

3.Glass (including vitrified or enamelled coatings or glass lining);

4.Graphite;

5.Nickel or alloys with more than 40% nickel by weight;

6.Tantalum or tantalum alloys;

7.Titanium or titanium alloys; or

8.Zirconium or zirconium alloys;

e.Distillation or absorption columns of internal diameter greater than 0.1 m, 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;

3.Glass (including vitrified or enamelled coatings or glass lining);

4.Graphite;

5.Nickel or alloys with more than 40% nickel by weight;

6.Tantalum or tantalum alloys;

7.Titanium or titanium alloys; or

8.Zirconium or zirconium 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.Multiple seal valves incorporating a leak detection port, bellows-seal valves, non-return (check) valves or diaphragm valves, in which 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;

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; or

7.Zirconium or zirconium alloys;

h.Multi-walled piping incorporating a leak detection port, in which 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;

3.Glass (including vitrified or enamelled coatings or glass lining);

4.Graphite;

5.Nickel or alloys with more than 40% nickel by weight;

6.Tantalum or tantalum alloys;

7.Titanium or titanium alloys; or

8.Zirconium or zirconium alloys;

i.Multiple-seal, canned drive, magnetic drive, bellows or diaphragm 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), 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;

2.Ceramics;

3.Ferrosilicon;

4.Fluoropolymers;

5.Glass (including vitrified or enamelled coatings or glass lining);

6.Graphite;

7.Nickel or alloys with more than 40% nickel by weight;

8.Tantalum or tantalum alloys;

9.Titanium or titanium alloys; or

10.Zirconium or zirconium alloys;

j.Incinerators designed to destroy chemicals specified in entry 1C350, having specially designed waste supply systems, special handling facilities and an average combustion chamber temperature greater than 1273 K (1000°C), in which all surfaces in the waste supply system that come into direct contact with the waste products are made from or lined with any of the following materials:

1.Alloys with more than 25% nickel and 20% chromium by weight;

2.Ceramics; or

3.Nickel or alloys with more than 40% nickel by weight.

2B351 Toxic gas monitoring systems, as follows, and dedicated detectors therefor:

a.Designed for continuous operation and usable for the detection of chemical warfare agents, chemicals specified in entry 1C350 or organic compounds containing phosphorus, sulphur, fluorine or chlorine, 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 biological manufacturing, as follows;

a.Containment facilities at Containment Level (ACDP) 3 or 4, and related equipment, as follows:

1.Facilities that meet the criteria for Containment Level 3 or 4 as specified in guidance from the Advisory Committee on Dangerous Pathogens approved by the Health and Safety Commission (published by HMSO, Second Edition 1990);

2.Independently ventilated protective full or half suits;

3.Biological safety cabinets or isolators, which allow manual operations to be performed within, whilst providing an environment equivalent to Class III biological protection;

Note: In this sub-head, “isolators” include flexible isolators, dry boxes, anaerobic chambers and glove boxes.

b.Fermenters, bioreactors, chemostats and continuous-flow systems, capable of operation without the propagation of aerosols, having all the following characteristics:

1.Capacity of 300 litres or more;

2.Double or multiple sealing joints within the steam containment area; and

3.Capable of in-situ sterilisation in a closed state;

c.Centrifugal separators or decanters, capable of continuous separation without the propagation of aerosols, having all the following characteristics:

1.Flow rate exceeding 100 litres per hour;

2.Components of polished stainless steel or titanium;

3.Double or multiple sealing joints within the steam containment area; and

4.Capable of in-situ sterilisation in a closed state;

d.Cross-flow filtration equipment, designed for continuous separation without the propagation of aerosols, having both of the following characteristics:

1.Equal to or greater than 5 square metres; and

2.Capable of in-situ sterilization;

e.Steam sterilisable freeze drying equipment with a condenser capacity exceeding 50 kg of ice in 24 hours and less than 1,000 kg of ice in 24 hours;

f.Chambers designed for aerosol challenge testing with pathogenic microorganisms or toxins and having a capacity of 1 m3 or greater.

2C  Materials

2D  Software

2D001 Software specially designed or modified for the development, production or use of goods specified in entries 2A001 to 2A006 or 2B001 to 2B009.

2D002 Specific software, as follows:

a.Software to provide adaptive control and having both of the following characteristics:

1.For flexible manufacturing units (FMUs) which consist at least of equipment described in sub-heads b.1. and b.2. of the definition of flexible manufacturing unit; and

2.Capable of generating or modifying, in real time processing, programmes or data by using the signals obtained simultaneously by means of at least two detection techniques, such as:

a.Machine vision (optical ranging);

b.Infrared imaging;

c.Acoustical imaging (acoustical ranging);

d.Tactile measurement;

e.Inertial positioning;

f.Force measurement;

g.Torque measurement;

b.Software for electronic devices other than those described in heads a. or b. of entry 2B001, which provides the numerical control capability of the goods specified in entry 2B001.

2D101 Software specially designed for the use of goods specified in entries 2B104, 2B115 or 2B116(22).

2D201 Software specially designed for the use of goods specified in entries 2B204, 2B207, 2B215, 2B227 or 2B229.

Technology

2E—2E001 Technology required for the development of goods specified in sub-categories 2A, 2B or 2D.

2E002 Technology required for the production of goods specified in sub-categories 2A or 2B.

2E003 Other technology, as follows:

a.Technology:

1.For the development of interactive graphics as an integrated part in numerical control units for preparation or modification of part programmes;

2.For the development of generators of machine tool instructions (e.g., part programmes) from design data residing inside numerical control units;

3.For the development of integration software for incorporation of expert systems for advanced decision support of shop floor operations into numerical control units;

b.Technology for metal-working manufacturing processes, as follows:

1.Technology for the design of tools, dies or fixtures specially designed for the following processes:

a.Superplastic forming;

b.Diffusion bonding;

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:

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.  Mixtures consist of 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.  MCrA1X 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 weight percent in various proportions and combinations;

a. CoCrAlY coatings which contain less than 22 weight percent of chromium, less than 7 weight percent of aluminium and less than 2 weight percent of yttrium;

b. CoCrAlY coatings which contain 22 to 24 weight percent of chromium, 10 to 12 weight percent of aluminium and 0.5 to 0.7 weight percent of yttrium; or

c. NiCrAlY coatings which contain 21 to 23 weight percent of chromium, 10 to 12 weight percent of aluminium and 0.9 to 1.1 weight percent of yttrium.

6.  The term “aluminium alloys” means alloys having an ultimate tensile strength of 190 MPa or more measured at 293 K (20°C).

7.  The term “corrosion resistant steel” means AISI (American Iron and Steel Institute) 300 series or equivalent national standard steels.

8.  Refractory metals consist of 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 and the following metal halides: potassium iodide, potassium fluoride, or sensor window materials of more than 40 mm diameter for thallium bromide and thallium chlorobromide.

10.  Technology for single-step pack cementation of solid airfoils is not specified in 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, etc., 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 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.  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.

1.CVD includes the following processes: directed gas flow out-of-pack deposition, pulsating CVD, controlled nucleation thermal decomposition (CNTD), plasma enhanced or plasma assisted CVD processes.

2.Pack denotes a substrate immersed in a powder mixture.

3.The gaseous reactants used in the out-of-pack process are produced using the same basic reactions and parameters as the pack cementation process, except: that the substrate to be coated is not in contact with the powder mixture.

b. 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.

c. Ion plating is a special modification of a general TE-PVD process in which a plasma or an ion source is used to ionize the species to be deposited, and a negative bias is applied to the substrate in order to facilitate the extraction of the species to be deposited from the plasma. The introduction of reactive species, evaporation of solids within the process chamber, and the use of monitors to provide in-process measurement of optical characteristics and thicknesses of coatings are ordinary modifications of the process.

d. Pack cementation is a surface modification coating or overlay coating process wherein a substrate is immersed in a powder mixture (a pack), that consists of:

1.The metallic powders that are to be deposited (usually aluminium, chromium, silicon or combinations thereof);

2.An activator (normally a halide salt); and

3.An inert powder, most frequently alumina.

e. 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 carried out underwater.

1.Low pressure means less than ambient atmospheric pressure.

2.High velocity refers to nozzle-exit gas velocity exceeding750 m/s calculated at 293 K (20°C) at 0.1 MPa.

f. Slurry deposition is a surface modification coating or overlay coating process wherein a metallic or ceramic powder with an organic binder is suspended in a liquid and is applied to a substrate by either spraying, dipping or painting, subsequent air or oven drying, and heat treatment to obtain the desired coating.

g. Sputter deposition is an overlay coating process based on a momentum transfer phenomenon, wherein positive ions are accelerated by an electric field towards the surface of a target (coating material). The kinetic energy of the impacting ions is sufficient to cause target surface atoms to be released and deposited on an appropriately positioned substrate.

1.The Table refers only to triode, magnetron or reactive sputter deposition which is used to increase adhesion of the coating and rate of deposition and to radio frequency (RF) augmented sputter deposition used to permit vaporization of non-metallic coating materials.

2.Low-energy ion beams (less than 5 keV) can be used to activatethe deposition.

h. Ion implantation is a surface modification coating process in which the element to be alloyed is ionized, accelerated through a potential gradient and implanted into the surface region of the substrate. This includes processes in which ion implantation is performed simultaneously with electron beam physical vapour deposition or sputter deposition.

2E101 Technology required for the use of equipment or software specified in entries 2B004, 2B104, 2B115, 2B116 or 2D101.

2E201 Technology required for the use of equipment or software specified in entries 2A225, 2A226, 2B001,2B006, head b. of entry 2B007, head c. of entry 2B007, or entries 2B008, 2B009, 2B204, 2B207, 2B215, 2B225 to 2B232 or 2D201.

2E301 Technology required for the use of goods specified in entries 2B350 to 2B352.

Category 3—Electronics
Equipment, Assemblies and Components

3A—3A Notes:

1.The control on export of equipment, devices and components described in entries 3A001 or 3A002, other than those described in sub-heads a.3. to a.10. or sub-head a.12. of entry 3A001, which are specially designed for, or which have the same functional characteristics as other equipment, is determined by the export control requirements applying to that other equipment.

2.The control on export of integrated circuits described in sub-heads a.3. to a.9. or sub-head a.12. of entry 3A001, which are unalterably programmed or designed for a specific function in a piece of equipment, is determined by the export control requirements applying to that other equipment.

1.When the export control requirements applying to the equipment cannot be determined, the integrated circuits are evaluated against the parameters in entry 3A001.

2.For silicon based microcomputer microcircuits or micro-controller microcircuits, having an operand (data) word length of 8 bits or less, the export control requirements thereof are determined only in sub-head a.3. of entry 3A001.

a. Electronic devices and components:

a.General purpose integrated circuits, as follows:

1.Wafers (finished or unfinished), in which the function has been determined, are evaluated against the parameters of this head.

2.Integrated circuits include the following types:

1.Integrated circuits, designed or rated as radiation hardened to withstand either of the following:

a.a total dose of 5 × 105 rads(Si), or higher; or

b.a dose rate upset of 5 × 108 rads(Si)/s or higher;

2.Microprocessor microcircuits, microcomputer microcircuits, microcontroller microcircuits, electrical erasable programmable read-only memories (EEPROMs), static random-access memories (SRAMs), storage integrated circuits manufactured from a compound semiconductor, analogue-to-digital converters, digital-to-analogue converters, electro-optical or optical integrated circuits for signal processing, field programmable gate arrays, field programmable logic arrays, neural network integrated circuits, 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, or Fast Fourier Transform (FFT) processors, as follows:

a.Rated for operation at an ambient temperature above 398 K (125°C);

b.Rated for operation at an ambient temperature below 218 K (-55°C); or

c.Rated for operation over the entire ambient temperature range from 218 K (-55°C) to 398 K (125°C);

3.Microprocessor microcircuits, microcomputer microcircuits and microcontroller microcircuits, having any of the following:Note: Sub-head a.3. of this entry includes digital signal processors, digital array processors and digital coprocessors.

a.An arithmetic logic unit with an access width of 32 bit or more and a composite theoretical performance (CTP) of 80 million theoretical operations per second (Mtops) or more;

b.Manufactured from a compound semiconductor and operating at a clock frequency exceeding 40 MHz; or

c.More than one data or instruction bus or serial communication port for external interconnection in a parallel processor with a transfer rate exceeding 2.5 Mbyte/s;

4.Electrically erasable programmable read-only memories (EEPROMs) static random-access memories (SRAMs) and storage integrated circuits manufactured from a compound semiconductor, as follows:

a.EEPROMs with a storage capacity:

1.Exceeding 16 Mbit per package for flash memory types; or

2.Exceeding either of the following limits for all other EEPROMtypes:

a.4 Mbit per package; or

b.1 Mbit per package and having a maximum access time of lessthan 80 ns;

b.SRAMs with a storage capacity:

1.Exceeding 4 Mbit per package; or

2.Exceeding 1 Mbit per package and having a maximum access time of less than 20 ns;

c.Storage integrated circuits manufactured from a compoundsemiconductor;

5.Analogue-to-digital and digital-to-analogue converter integrated circuits, as follows:

a.Analogue-to-digital converters having any of the following:

1.A resolution of 8 bit or more, but less than 12 bit, with a total conversion time to maximum resolution of less than 10 ns;

2.A resolution of 12 bit with a total conversion time to maximumresolution of less than 200 ns; or

3.A resolution of more than 12 bit with a total conversion time to maximum resolution of less than 2 microseconds;

b.Digital-to-analogue converters with a resolution of 12 bit or more, and a settling time of less than 10 ns;

6.Electro-optical or optical integrated circuits for signal processing having all of the following:

a.One or more internal laser diodes;

b.One or more internal light detecting elements; and

c.Optical waveguides;

7.Field programmable gate arrays having either of the following:

a.An equivalent usable gate count of more than 30,000 (2 input gates); or

b.A typical basic gate propagation delay time of less than 0.4 ns;

8.Field programmable logic arrays having either of the following:

a.An equivalent usable gate count of more than 30,000 (2 input gates); or

b.A toggle frequency exceeding 133 MHz;

9.Neural network integrated circuits;

10.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, having any of the following:

a.More than 144 terminals;

b.A typical basic gate propagation delay time of less than 0.4 ns; or

c.An operating frequency exceeding 3 GHz;

11.Digital integrated circuits based upon any compound semiconductor and having either of the following:

a.An equivalent gate count of more than 300 (2 input gates); or

b.A toggle frequency exceeding 1.2 GHz;

12.Fast Fourier Transform (FFT) processors having any of the following:

a.A rated execution time for a 1,024 point complex FFT of less than 1 ms;

b.A rated execution time for an N-point complex FFT of other than 1,024 points of less than N log2 N/10,240 ms, where N is the number of points; or

c.A butterfly throughput of more than 5.12 MHz;

b.Microwave or millimetre wave devices:

1.Electronic vacuum tubes and cathodes, as follows:

a.

Travelling wave tubes, pulsed or continuous wave, as follows:

1.

Operating at frequencies higher than 31 GHz;

2.

Having a cathode heater element with a turn on time to rated RF power of less than 3 seconds;

3.

Coupled cavity tubes, or derivatives thereof with an instantaneous bandwidth of more than 7% or a peak power exceeding 2.5 kW;

4.

Helix tubes, or derivatives thereof, with any of the following characteristics:

a.

An instantaneous bandwidth of more than one octave, and average power (expressed in kW) times frequency (expressed in GHz) of more than 0.5;

b.

An instantaneous bandwidth of one octave or less, and average power (expressed in kW) times frequency (expressed in GHz) of more than 1; or

c.

Space qualified;

b.

Crossed-field amplifier tubes with a gain of more than 17 dB;

c.

Impregnated cathodes for electronic tubes, with either of the following:

1.

Having a turn on time to rated emission of less than 3 seconds; or

2.

Producing a continuous emission current density at rated operating conditions exceeding 5 A/cm2;

2.Microwave integrated circuits or modules containing monolithic integrated circuits operating at frequencies exceeding 3 GHz;

3.Microwave transistors rated for operation at frequencies exceeding 31 GHz;

4.Microwave solid state amplifiers, as follows:

a.Operating at frequencies exceeding 10.5 GHz and having an instantaneous bandwidth of more than half an octave;

b.Operating at frequencies exceeding 31 GHz;

5.Electronically or magnetically tunable band-pass or band-stop filters having more than 5 tunable resonators capable of tuning across a 1.5:1 frequency band (fmax/fmin) in less than 10 microseconds with either:

a.A band-pass bandwidth of more than 0.5% of centre frequency; or

b.A band-stop bandwidth of less than 0.5% of centre frequency;

6.Microwave assemblies capable of operating at frequencies exceeding 31 GHz;

7.Mixers and converters designed to extend the frequency range of equipment described in heads c., e. or f. of entry 3A002 beyond the limits stated therein;

c.Acoustic wave devices, as follows, and specially designed components therefor:

1.Surface acoustic wave and surface skimming (shallow bulk) acoustic wave devices (i.e., signal processing devices employing elastic waves in materials), having any of the following:

a.A carrier frequency exceeding 2.5 GHz;

b.A carrier frequency of 2.5 GHz or less, and:

1.A frequency side-lobe rejection exceeding 55 dB;

2.A product of the maximum delay time and the bandwidth (time in microseconds and bandwidth in MHz) of more than 100; or

3.A dispersive delay of more than 10 microseconds; or

c.A carrier frequency exceeding 1 GHz and a bandwidth of 250 MHz or more;

2.Bulk (volume) acoustic wave devices (i.e., signal processing devices employing elastic waves) which permit direct processing of signals at frequencies exceeding 1 GHz;

3.Acoustic-optic signal processing devices employing interaction between acoustic waves (bulk wave or surface wave) and light waves which permit the direct processing of signals or images, including spectral analysis, correlation or convolution;

d.Electronic devices or circuits containing components, manufactured from superconductive materials specially designed for operation at temperatures below the critical temperature of at least one of the superconductive constituents, with any of the following:

1.Electromagnetic amplification:

a.At frequencies equal to or less than 31 GHz with a noise figure of less than 0.5 dB; or

b.At frequencies exceeding 31 GHz;

2.Current switching for digital circuits using superconductive gates with a product of delay time per gate (in seconds) and power dissipation per gate (in watts) of less than 10−14 J; or

3.Frequency selection at all frequencies using resonant circuits with Q-values exceeding 10,000;

e.High energy devices, as follows:

1.Batteries, as follows:

a.Primary cells and batteries having an energy density exceeding 480 Wh/kg and rated for operation in the temperature range from below 243 K (-30°C) to above 343 K (70°C);

b.Rechargeable cells and batteries having an energy density exceeding 150 Wh/kg after 75 charge/discharge cycles at a discharge current equal to C/5 hours (C being the nominal capacity in ampere hours) when operating in the temperature range from below 253 K (-20°C) to above 333 K (60°C);

c.Space qualified and radiation hardened photovoltaic arrays with a specific power exceeding 160 W/m2 at an operating temperature of 301 K (28°C) under a tungsten illumination of 1 kW/m2 at 2,800 K (2,527°C);

2.High energy storage capacitors, as follows(23):

a.Capacitors with a repetition rate of less than 10 Hz (single shot capacitors) having all of the following:

1.A voltage rating equal to or more than 5 kV;

2.An energy density equal to or more than 250 J/kg; and

3.A total energy equal to or more than 25 kJ;

b.Capacitors with a repetition rate of 10 Hz or more (repetition rated capacitors) having all of the following:

1.A voltage rating equal to or more than 5 kV;

2.An energy density equal to or more than 50 J/kg;

3.A total energy equal to or more than 100 J; and

4.A charge/discharge cycle life equal to or more than 10,000;

3.Superconductive electromagnets or solenoids specially designed to be fully charged or discharged in less than one second, having all of the following(24):

a.Energy delivered during the discharge exceeding 10 kJ in the first second;

b.Inner diameter of the current carrying windings of more than 250 mm; and

c.Rated for a magnetic induction of more than 8 T or overall current density in the winding of more than 300 A/mm2;

4.Circuits or systems for electromagnetic energy storage, containing components manufactured from superconductive materials specially designed for operation at temperatures below the critical temperature of at least one of their superconductive constituents, having all of the following:

a.Resonant operating frequencies exceeding 1 MHz;

b.A stored energy density of 1 MJ/m3 or more; and

c.A discharge time of less than 1 ms;

5.Flash discharge type X-ray systems, and tubes therefor, having all of the following(25):

a.A peak power exceeding 500 MW;

b.An output voltage exceeding 500 kV; and

c.A pulse width of less than 0.2 microsecond;

f.Rotary input type shaft absolute position encoders having either of the following:

1.A resolution of better than 1 part in 265,000 (18 bit resolution) of full scale; or

2.An accuracy better than ± 2.5 seconds of arc.

3A002 General purpose electronic equipment:

a.Recording equipment, as follows, and specially designed test tape therefor:

1.Analogue instrumentation magnetic tape recorders, including those permitting the recording of digital signals (e.g., using a high density digital recording (HDDR) module), having any of the following:

a.A bandwidth exceeding 4 MHz per electronic channel or track;

b.A bandwidth exceeding 2 MHz per electronic channel or track and having more than 42 tracks; or

c.A time displacement (base) error, measured in accordance with applicable Inter Range Instrumentation Group (IRIG) or Electronic Industries Association (EIA) documents, of less than ± 0.1 microsecond;

2.Digital video magnetic tape recorders having a maximum digital interface transfer rate exceeding 180 Mbit/s, except: those specially designed for television recording using a signal format standardized or recommended by the International Radio Consultative Committee (CCIR) or the International Technical Commission (IEC) for civil television applications;

3.Digital instrumentation magnetic tape data recorders employing helical scan techniques or fixed head techniques, having either of the following:

a.A maximum digital interface transfer rate exceeding 175 Mbit/s; or

b.Space qualified;

4.Equipment, with a maximum digital interface transfer rate exceeding 175 Mbit/s, designed to convert digital video magnetic tape recorders for use as digital instrumentation data recorders;

5.Waveform digitisers and transient recorders with both of the following(26):

a.Digitising rates equal to or more than 200 million samples per second and a resolution of 10 bits or more; and

b.A continuous throughput of 2 Gbits/s or more;

b.Frequency synthesiser electronic assemblies having a frequency switching time from one selected frequency to another of less than 1 ms;

c.Signal analysers, as follows:

1.Capable of analysing frequencies exceeding 31 GHz;

2.Dynamic signal analysers with a real-time bandwidth exceeding 25.6 kHz; except:

d.Frequency synthesised signal generators producing output frequencies, the accuracy and short term and long term stability of which are controlled, derived from or disciplined by the internal master frequency, and having any of the following:

1.A maximum synthesised frequency exceeding 31 GHz;

2.A frequency switching time from one selected frequency to another of less than 1 ms; or

3.A single sideband (SSB) phase noise better than -(126 + 20 log10F − 20 log10f) in dBc/Hz, where F is the off-set from the operating frequency in Hz and f is the operating frequency in MHz;

e.Network analysers with a maximum operating frequency exceeding 31 GHz;

f.Microwave test receivers with both of the following:

1.A maximum operating frequency exceeding 31 GHz; and

2.Capable of measuring amplitude and phase simultaneously;

g.Atomic frequency standards having either of the following characteristics:

1.Long term stability (aging) less (better) than 1 × 10−11/month; or

2.Space qualified;

h.Emulators for microcircuits specified in sub-heads a.3. or a.9. of entry 3A001.

3A101 Electronic devices and components, other than those specified in entry 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.

3A201 Electronic devices and components, other than those specified in entry 3A001, as follows:

a.Capacitors with the following characteristics:

1.Voltage rating greater than 1.4 kV, energy storage greater than 10J, capacitance greater than 500 nF and series inductance less than 50 nH; or

2.Voltage rating greater than 750 V, capacitance greater than 250 nF and series inductance less than 10 nH;

b.Superconducting solenoidal electromagnets with all of the following characteristics:

1.Capable of creating magnetic fields of more than 2 Teslas (20 kilogauss);

2.With an L/D ratio (length divided by inner diameter) greater than 2;

3.With an inner diameter of more than 300 mm; and

4.With a magnetic field uniform to better than 1% over the central 50% of the inner volume.

Note: Head b. of this entry does not specify magnets specially designed for and exported as parts of medical nuclear magnetic resonance (NMR) imaging systems. In this entry, “as part of” does not necessarily mean physical part in the same shipment; separate shipments from different sources are allowed, provided the related export documents clearly specify that the shipments are dispatched “as part of” the same imaging systems.

c.Flash X-ray generators or pulsed electron accelerators with peak energy of 500 keV or greater, as follows;

3A202 Oscilloscopes and transient recorders other than those specified in sub-head a.5. of entry 3A002, as follows; and specially designed components therefor:

a.Non-modular analogue oscilloscopes having a bandwidth of 1 GHz or greater;

b.Modular analogue oscilloscope systems having either of the following characteristics:

1.A mainframe with a bandwidth of 1 GHz or greater; or

2.Plug-in modules with an individual bandwidth of 4 GHz or greater;

c.Analogue sampling oscilloscopes for the analysis of recurring phenomena with an effective bandwidth greater than 4 GHz;

d.Digital oscilloscopes and transient recorders, using analogue-to-digital conversion techniques, capable of storing transients by sequentially sampling single-shot inputs at successive intervals of less than 1 ns (greater than 1 giga-sample per second), digitizing to 8 bits or greater resolution and storing 256 or more samples.

1.Specially designed components specified in this entry are the following, for analogue oscilloscopes:

a.Plug-in units;

b.External amplifiers;

c.Pre-amplifiers;

d.Sampling devices;

e.Cathode ray tubes.

2.In this entry, the term “bandwidth” means the band of frequencies over which the deflection on the cathode ray tube does not fall below 70.7% of that at the maximum point measured with a constant input voltage to the oscilloscope amplifier.

3A225 Frequency changers (also known as converters or inverters) or generators, other than those specified in entry B10b.2.k. of Group 2 of Part III of this Schedule, having all of the following characteristics:

a.A multiphase output capable of providing a power of 40 W or more;

b.Capable of operating in the frequency range between 600 and 2000 Hz;

c.Total harmonic distortion below 10%; and

d.Frequency control better than 0.1%.

3A226 Direct current high-power supplies capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater and with current or voltage regulation better than 0.1%.

3A227 High-voltage direct current power supplies capable of continuously producing, over a time period of 8 hours, 20,000 V or greater with current output of 1 A or greater and with current or voltage regulation better than 0.1%.

3A228 Switching devices, as follows:

a.Cold-cathode tubes (including gas krytron tubes and vacuum sprytron tubes), whether gas filled or not, operating similarly to a spark gap, containing three or more electrodes, and having all of the following characteristics:

1.Anode peak voltage rating of 2,500 V or more;

2.Anode peak current rating of 100 A or more; and

3.Anode delay time of 10 microsecond or less;

b.Triggered spark-gaps having an anode delay time of 15 microsecond or less and rated for a peak current of 500 A or more;

c.Modules or assemblies with a fast switching function having all of the following characteristics:

1.Anode peak voltage rating greater than 2,000 V;

2.Anode peak current rating of 500 A or more; and

3.Turn-on time of 1 microsecond or less.

3A229 Firing sets and equivalent high-current pulse generators (for controlled detonators), as follows(27):

a.Explosive detonator firing sets designed to drive multiple controlled detonators specified in entry 3A232;

b.Modular electrical pulse generators (pulsers) designed for portable, mobile or ruggedized use (including xenon flash-lamp drivers) having all the following characteristics:

1.Capable of delivering their energy in less than 15 microsecond;

2.Having an output greater than 100 A;

3.Having a rise time of less than 10 microsecond into loads of less than 40 ohms (rise time is the time interval from 10% to 90% current amplitude when driving a resistive load);

4.Enclosed in a dust-tight enclosure;

5.No dimension greater than 254 mm;

6.Weight less than 25 kg; and

7.Specified for use over an extended temperature range (223 K [-50°C] to 373 K [100°C]) or specified as suitable for aerospace use.

3A230 High-speed pulse generators with output voltages greater than 6 volts into a less than 55 ohm resistive load, and with pulse transition times less than 500 picoseconds.

In this entry, “pulse transition time” means the time interval between 10% and 90% voltage amplitude.

3A231 Neutron generator systems, including tubes, designed for operation without an external vacuum system and utilizing electrostatic acceleration to induce a tritium-deu-terium nuclear reaction.

3A232 Detonators and multipoint initiation systems, as follows(28):

a.Electrically driven explosive detonators, the following:

1.Exploding bridge (EB);

2.Exploding bridge wire (EBW);

3.Slapper;

4.Exploding foil initiators (EFI);

b.Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface (over greater than 5000 mm2) from a single firing signal (with an initiation timing spread over the surface of less than 2.5 microseconds).

1.This entry does not specify detonators using only primary explosives, such as lead azide.

2.The detonators in this entry all utilise a small electrical conductor (bridge, bridge wire or foil) that explosively vaporizes when a fast, high-current electrical pulse is passed through it. In nonslapper 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 a magnetic force. The term 'exploding foil' detonator may refer to either an EB or a slapper-type detonator.

3A233 Mass spectrometers, other than those specified in entry B20g. of Group 2 of Part III of this Schedule, 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 which have a source chamber constructed from, lined with or plated with materials resistant to UF6;

e.Molecular beam mass spectrometers as follows:

1.Which have a source chamber constructed from, lined with or plated with stainless steel or molybdenum and have a cold trap capable of cooling to 193 K (-80°C) or less; or

2.Which have a source chamber constructed from, lined with or plated with materials resistant to UF6; or

f.Mass spectrometers equipped with a microfluorination ion source designed for use with actinides or actinide fluorides.

3A990 Apparatus or devices, other than those specified in entry PL5006 of Group 1 of Part III of this Schedule or entries 3A229 to 3A232 of this Group, designed for the handling, control, discharging, decoying, jamming, detonation, disruption or detection of explosive devices or improvised explosive devices;

3B  Test, Inspection and Production Equipment

3B Equipment for the manufacture or testing of semiconductor devices or materials, as follows, and specially designed components and accessories therefor:

3B001 Stored programme controlled equipment for epitaxial growth, as follows:

a.Capable of producing a layer thickness uniform to less than ± 2.5% across a distance of 75 mm or more;

b.Metal organic chemical vapour deposition (MOCVD) reactors specially designed for compound semiconductor crystal growth by the chemical reaction between materials specified in entries 3C003 or 3C004;

c.Molecular beam epitaxial growth equipment using gas sources.

3B002 Stored programme controlled equipment designed for ion implantation, having any of the following:

a.An accelerating voltage exceeding 200 keV;

b.Specially designed and optimized to operate at an accelerating voltage of less than 10 keV;

c.Direct write capability; or

d.Capable of high energy oxygen implant into a heated semiconductor material substrate.

3B003 Stored programme controlled anisotropic plasma dry etching equipment, as follows:

a.With cassette-to-cassette operation and load-locks, and having either of the following:

1.Magnetic confinement; or

2.Electron cyclotron resonance (ECR);

b.Specially designed for equipment specified in entry 3B005 and having either of the following:

1.Magnetic confinement; or

2.Electron cyclotron resonance (ECR).

3B004 Stored programme controlled plasma enhanced CVD equipment, as follows:

a.With cassette-to-cassette operation and load-locks, and having either of the following:

1.Magnetic confinement; or

2.Electron cyclotron resonance (ECR);

b.Specially designed for equipment specified in entry 3B005 and having either of the following:

1.Magnetic confinement; or

2.Electron cyclotron resonance (ECR).

3B005 Stored programme controlled automatic loading multi-chamber central wafer handling systems, having interfaces for wafer input and output, to which more than two pieces of semiconductor processing equipment are to be connected, to form an integrated system in a vacuum environment for sequential multiple wafer processing.

3B006 Stored programme controlled lithography equipment, as follows:

a.Align and expose step and repeat equipment for wafer processing using photo-optical or X-ray methods, having either of the following:

1.A light source wavelength shorter than 400 nm; or

2.Capable of producing a pattern with a minimum resolvable feature size of 0.7 micrometre or less when calculated by the following formula:

where:

  • “MRF” means the minimum resolvable feature size;

  • the “K factor” = 0.7; and

  • “wavelength” means the exposure light source wavelength;

b.Equipment specially designed for mask making or semiconductor device processing using deflected focussed electron beam, ion beam or laser beam, with any of the following:

1.A spot size smaller than 0.2 micrometre;

2.Capable of producing a pattern with a feature size of less than 1 micrometre; or

3.An overlay accuracy of better than ± 0.20 micrometre (3 sigma).

3B007 Masks or reticles, as follows:

a.For integrated circuits specified in entry 3A001;

b.Multi-layer masks with a phase shift layer.

3B008 Stored programme controlled test equipment, specially designed for testing semiconductor devices and unencapsulated dice, as follows:

a.For testing S-parameters of transistor devices at frequencies exceeding 31 GHz;

b.For testing integrated circuits, and capable of performing functional (truth table) testing at a pattern rate of more than 40 MHz;

1.Electronic assemblies or a class of electronic assemblies for home or entertainment applications;

2.Electronic components, electronic assemblies or integrated circuits not specified in this Group.

c.For testing microwave integrated circuits at frequencies exceeding 3 GHz;

d.Electron beam systems designed for operation at or below 3 keV, or laser beam systems, for the non-contactive probing of powered-up semiconductor devices, with both of the following:

1.Stroboscopic capability with either beam-blanking or detector strobing; and

2.An electron spectrometer for voltage measurement with a resolution of less than 0.5 V.

3C  Materials

3C001 Hetero-epitaxial materials consisting of a substrate with stacked epitaxially grown multiple layers of:

a.Silicon;

b.Germanium; or

c.III/V compounds of gallium or indium.

3C002 Resist materials, as follows, and substrates coated with controlled resists:

a.Positive resists for semiconductor lithography specially adjusted (optimised) for use at wavelengths below 370 nm;

b.All resists, for use with electron beams or ion beams, with a sensitivity of 0.01 microcoulomb/mm2 or better;

c.All resists, for use with X-rays, with a sensitivity of 2.5 mJ/mm2 or better;

d.All resists optimized for surface imaging technologies, including silylated resists.

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%.

3C004 Hydrides of phosphorus, arsenic or antimony, having a purity better than 99.999%, even diluted in inert gases or hydrogen.

3D  Software

3D001 Software specially designed for the development or production of goods specified in head b. of entry 3A001 to head h. of entry 3A002 or Sub-category 3B.

3D002 Software specially designed for the use of stored programme controlled equipment specified in sub-category 3B.

3D003 Computer-aided-design (CAD) software for semiconductor devices or integrated circuits, having any of the following:

a.Design rules or circuit verification rules;

b.Simulation of the physically laid out circuits; or

c.Lithographic processing simulators for design.

3D101 Software specially designed for the use of goods specified in head b. of entry 3A101.

3E  Technology

3E001 Technology required for the development or production of goods specified in sub-categories 3A, 3B or 3C;

a.Microwave transistors operating at frequencies below 31 GHz;

b.Integrated circuits specified in sub-heads a.3. to a.12. of entry 3A001, having both of the following characteristics:

1.Using technology of one micrometre or more; and

2.Not incorporating multi-layer structures.

3E002 Other technology for the development or production of:

a.Vacuum microelectronic devices;

b.Hetero-structure semiconductor devices such as high electron mobility transistors (HEMT), hetero-bipolar transistors (HBT), quantum well or super lattice devices;

c.Superconductive electronic devices;

d.Substrates of films of diamond for electronic components.

3E101 Technology required for the use of goods specified in sub-heads a.1. or a.2. of entry 3A001, entries 3A101 or 3D101.

3E102 Technology required for the development of software specified in entry 3D101.

3E201 Technology required for the use of goods specified in sub-head e.2. of entry 3A001, sub-head e.3. of entry 3A001, sub-head e.5. of entry 3A001, or entries 3A201, 3A202, 3A225 to 3A233.

3E990 Technology required for the use of goods specified in entry 3A990.

Category 4—Computers
Notes:

1. In order to determine the export control requirements on computers, related equipment or software performing telecommunications or local area network functions they must also be evaluated against Category 5 (Part 1 – Telecommunications).

1.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).

2.Software which provides routing or switching of datagram or fast select packets (i.e., packet by packet route selection) or of software specially designed for packet switching, is specified in Category 5 (Part 1 – Telecommunications).

2. Computers, related equipment or software performing cryptographic, cryptanalytic, certifiable multilevel 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  Equipment, Assemblies and Components

4A001 Electronic computers and related equipment, as follows, and electronic assemblies and specially designed components therefor(29):

a.Specially designed to have either of the following characteristics:

1.Rated for operation at an ambient temperature below 228 K (-45°C) or above 358 K (85°C); or

2.Radiation hardened to exceed any of the following specifications:

a.Total Dose 5 × 105 Rads (Si);

b.Dose Rate Upset 5 × 108 Rads (Si)/sec; or

c.Single Event Upset 1 × 10−7 Error/bit/day;

b.Having characteristics or performing functions exceeding the limits in Category 5 (Part 2—Information Security).

4A002 Hybrid computers, as follows, and electronic assemblies and specially designed components therefor(30):

a.Containing digital computers specified in entry 4A003;

b.Containing analogue-to-digital converters having both of the following characteristics:

1.32 channels or more; and

2.A resolution of 14 bits (plus sign bit) or more with a conversion rate of 200,000 conversions/s or more.

4A003 Digital computers, electronic assemblies, and related equipment therefor, as follows, and specially designed components therefor:

a.Designed or modified for fault tolerance;

b.Digital computers having a composite theoretical performance (CTP) exceeding 260 million theoretical operations per second (Mtops);

c.Electronic assemblies specially designed or modified to be capable of enhancing performance by aggregation of computing elements so that the composite theoretical performance (CTP) of the aggregation exceeds the limit in head b. of this entry;

d.Graphics accelerators or graphics coprocessors exceeding a 3-D vector rate of 1,600,000;

e.Equipment performing analogue-to-digital conversions exceeding the limits in sub-head a.5. of entry 3A001;

f.Equipment containing terminal interface equipment exceeding the limits in sub-head b.3. of entry 5A001;

g.Equipment specially designed to provide for the external interconnection of digital computers or associated equipment which allows communications at data rates exceeding 80 Mbytes/s.

4A004 Computers, as follows, and specially designed related equipment, electronic assemblies and components therefor:

a.Systolic array computers;

b.Neural computers;

c.Optical computers.

4A101 Analogue computers, digital computers or digital differential analysers, other than those specified in sub-head a.1. of entry 4A001, which are ruggedized and designed or modified for use in systems specified in entries 9A004 or 9A104.

4A102 Hybrid Computers specially designed for modelling, simulation or design integration of systems specified in entries 9A004 or 9A104.

4B  Test, Inspection and Production Equipment

4C  Materials

4D  Software

4D001 Software specially designed or modified for the development, production or use of goods specified in entries 4A001 to 4A004, or sub-category 4D.

4D002 Software specially designed or modified to support technology specified in subcategory 4E.

4D003 Specific software, as follows:

a.Operating system software, software development tools and compilers specially designed for multi-data-stream processing equipment, in source code;

b.Expert systems or software for expert system inference engines providing both:

1.Time dependent rules; and

2.Primitives to handle the time characteristics of the rules and the facts;

c.Software having characteristics or performing functions exceeding the limits in Category 5 (Part 2-Information Security);

d.Operating systems specially designed for real time processing equipment which guarantees a global interrupt latency time of less than 20 microseconds.

4E  Technology

4E001 Technology required for the development, production or use of goods specified in sub-categories 4A or 4D.

4E002 a. Technology for the development or production of goods designed for multi-data-stream processing where the composite theoretical performance (CTP) exceeds 120 Mtops;

b.Technology required for the development or production of magnetic hard disk drives with a maximum bit transfer rate exceeding 47 Mbit/s.

Category 5 —Telecommunications and Information Security
(1)

See also entries 1A202, 9A010 and 9A110.

(2)

See also entry 9A110.

(3)

See also entries 1B101 and 1B201.

(4)

See also entry 1B201.

(5)

See also entry 1C101.

(6)

See also entry 1C202.

(7)

See also entry 1C107.

(8)

See also entry 1C210.

(9)

See also entry 1C216.

(10)

See also entry 1C991.

(11)

See also ML7 of Group 1 of Part III of this Schedule.

(12)

See also ML7 of Group 1 of Part III of this Schedule.

(13)

See also entry 1C992.

(14)

See also ML7 of Group 1 of Part III of this Schedule.

(15)

O.J. No. L167, 22.6.92 p.1.

(16)

See also ML7 of Group 1 of Part III of this Schedule.

(17)

See also entries 1C115, 1C239 and ML8 of Group 1 of Part III of this Schedule.

(18)

See also Entries 2B104 and 2B204.

(19)

See also entry 2B207.

(20)

See also entry 2B215.

(21)

See also sub-category 3B.

(22)

See also entry 9D004.a.

(23)

See also entry 3A201.a.

(24)

See also entry 3A201.b.

(25)

See also entry 3A101.b. and 3A201.c.

(26)

See also entry 3A202.

(27)

See also Group 1 of Part III of this Schedule.

(28)

See also Group 1 of Part III of this Schedule.

(29)

See also entry 4A101.

(30)

See also entry 4A102.