Council Regulation (EC) No 423/2007 (repealed)Show full title

[F1 I.6 SENSORS AND LASERS U.K.

I.6A

Goods

a The texts of points a, b and c in this entry do not correspond with those of points a, b and c of 6A005.
No	Relevant item(s) from Annex to Regulation (EC) No 1183/2007	Description
I.6A.001	ex 6A005.b*, ex 6A005.c* and ex 6A005.d* a.: ex 6A005.d.4 b.: ex 6A005.b.2-4 c.: ex 6A005.c.2	‘Lasers’, other than those specified in I.0A.002.g.5. or I.0A.002.h.6., components and optical equipment, as follows: a a. Pulsed excimer (XeF, XeCl, KrF) ‘ lasers ’ having all of the following characteristics: 1. Operating at wavelengths between 240 nm and 360 nm; 2. A repetition rate greater than 250 Hz; and 3. An average output power exceeding 500 W. b. Copper (Cu) vapour ‘ lasers ’ having both of the following characteristics: 1. Operating at wavelengths between 500 nm and 600 nm; and 2. An average output power exceeding 40 W. c. Solid state ‘tunable’ alexandrite (CR: BeAl 2 O 4 ) ‘lasers’ having all of the following characteristics: 1. Operating at wavelengths between 720 nm and 800 nm; 2. A bandwidth of 0,005 nm or less; 3. A repetition rate greater than 125 Hz; and 4. An average output power exceeding 30 W.
I.6A.002	6A007.c	Gravity gradiometers.
I.6A.003	6A102	Radiation hardened ‘detectors’ specially designed or modified for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects) and usable for ‘missiles’, designed or rated to withstand radiation levels which meet or exceed a total irradiation dose of 5 × 10 5 rads (silicon). Technical Notes: In I.6A.003, a ‘ detector ’ is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure.
I.6A.004	6A107	Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows: a. Gravity meters, designed or modified for airborne or marine use, and having a static or operational accuracy of 7 × 10 -6 m/s 2 (0,7 milligal) or less (better), and having a time-to-steady-state registration of two minutes or less; b. Specially designed components for gravity meters specified in I.6A.004.a. and gravity gradiometers specified in I.6A.002.
I.6A.005	6A108	Radar systems and tracking systems as follows: a. Radar and laser radar systems designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005; N.B.: See also Military Goods Controls for radar and laser systems for rockets or missiles. Note: I.6A.005.a. includes the following: a. Terrain contour mapping equipment; b. Imaging sensor equipment; c. Scene mapping and correlation (both digital and analogue) equipment; d. Doppler navigation radar equipment. b. Precision tracking systems, usable for ‘ missiles ’ , as follows: 1. Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity; 2. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities: a. Angular resolution better than 3 milliradians; b. Range of 30 km or greater with a range resolution better than 10 m rms; c. Velocity resolution better than 3 m/s. Technical Notes: In I.6A.005.b. ‘ missile ’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
I.6A.006	6A202	Photomultiplier tubes having both of the following characteristics: a. Photocathode area of greater than 20 cm 2 ; and b. Anode pulse rise time of less than 1 ns.
I.6A.007	6A203	Cameras and components, as follows: a. Mechanical rotating mirror cameras, as follows, and specially designed components therefor: 1. Framing cameras with recording rates greater than 225 000 frames per second; 2. Streak cameras with writing speeds greater than 0,5 mm per microsecond; Note: In I.6A.007.a. components of such cameras include their synchronizing electronics units and rotor assemblies consisting of turbines, mirrors and bearings. b. Electronic streak cameras, electronic framing cameras, tubes and devices, as follows: 1. Electronic streak cameras capable of 50 ns or less time resolution; 2. Streak tubes for cameras specified in I.6A.007.b.1.; 3. Electronic (or electronically shuttered) framing cameras capable of 50 ns or less frame exposure time; 4. Framing tubes and solid-state imaging devices for use with cameras specified in I.6A.007.b.3., as follows: a. Proximity focused image intensifier tubes having the photocathode deposited on a transparent conductive coating to decrease photocathode sheet resistance; b. Gate silicon intensifier target (SIT) videcon tubes, where a fast system allows gating the photoelectrons from the photocathode before they impinge on the SIT plate; c. Kerr or Pockels cell electro-optical shuttering; d. Other framing tubes and solid-state imaging devices having a fast-image gating time of less than 50 ns specially designed for cameras specified in I.6A.007.b.3.; c. Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 50 × 10 3 Gy(silicon) (5 × 10 6 rad (silicon)) without operational degradation. Technical Notes: The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation
I.6A.008	6A205	‘ Lasers ’ , ‘ laser ’ amplifiers and oscillators, other than those specified in I.0A.002.g.5., I.0A.002.h.6. and I.6A.001; as follows: a. Argon ion ‘ lasers ’ having both of the following characteristics: 1. Operating at wavelengths between 400 nm and 515 nm; and 2. An average output power greater than 40 W; b. Tunable pulsed single-mode dye laser oscillators having all of the following characteristics: 1. Operating at wavelengths between 300 nm and 800 nm; 2. An average output power greater than 1 W; 3. A repetition rate greater than 1 kHz; and 4. Pulse width less than 100 ns; c. Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics: 1. Operating at wavelengths between 300 nm and 800 nm; 2. An average output power greater than 30 W; 3. A repetition rate greater than 1 kHz; and 4. Pulse width less than 100 ns; Note: I.6A.008.c. does not prohibit single mode oscillators; d. Pulsed carbon dioxide ‘ lasers ’ having all of the following characteristics: 1. Operating at wavelengths between 9 000 nm and 11 000 nm; 2. A repetition rate greater than 250 Hz; 3. An average output power greater than 500 W; and 4. Pulse width of less than 200 ns; e. Para-hydrogen Raman shifters designed to operate at 16 micrometre output wavelength and at a repetition rate greater than 250 Hz; f. Neodymium-doped (other than glass) ‘ lasers ’ , having an output wavelength exceeding 1 000 nm but not exceeding 1 100 nm, as follows: 1. Pulse-excited, ‘ Q-switched lasers ’ having a ‘ pulse duration ’ equal to or more than 1 ns, and having either of the following: a. A single-transverse mode output having an average output power exceeding 40 W; or b. A multiple-transverse mode output having an average power exceeding 50 W; or 2. Incorporating frequency doubling to give an output wavelength of 500 nm or more but not exceeding 550 nm and having an average output power exceeding 40 W.
I.6A.009	6A225	Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds. Note: I.6A.009 includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers).
I.6A.010	6A226	Pressure sensors, as follows: a. Manganin gauges for pressures greater than 10 GPa; b. Quartz pressure transducers for pressures greater than 10 GPa
I.6A.011	ex 6B108*	Systems specially designed for radar cross section measurement usable for ‘ missiles ’ and their subsystems.

I.6B

Technology, including software

No	Relevant item(s) from Annex to Regulation (EC) No 1183/2007	Description
I.6B.001	6D102	‘ Software ’ specially designed or modified for the ‘ use ’ of goods specified in I.6A.005.
I.6B.002	6D103	‘ Software ’ which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for ‘ missiles ’ . Technical Notes: In I.6B.002 ‘ missile ’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
I.6B.003	ex 6E001	‘ Technology ’ according to the General Technology Note for the ‘ development ’ of equipment, materials or ‘ software ’ specified in I.6A.001, I.6A.002.c, I.6A.003, I.6A.004 to I.6A.010, I.6B.001 or I.6B.002.
I.6B.004	ex 6E002	‘ Technology ’ according to the General Technology Note for the ‘ production ’ of equipment or materials specified in I.6A.001, I.6A.002.c or I.6A.003 to I.6A.010.
I.6B.005	ex 6E101	‘ Technology ’ according to the General Technology Note for the ‘ use ’ of equipment or ‘ software ’ specified in I.6A.002 to I.6A.005, I.6A.011, I.6B.001 or I.6B.002.
I.6B.006	ex 6E201	‘ Technology ’ according to the General Technology Note for the ‘ use ’ of equipment specified in I.6A.001 or I.6A.006 to I.6A.010.]

Textual Amendments

F1 Substituted by Commission Regulation (EC) No 116/2008 of 28 January 2008 amending Council Regulation (EC) No 423/2007 concerning restrictive measures against Iran.