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Council Regulation (EC) No 423/2007 of 19 April 2007 concerning restrictive measures against Iran (repealed)
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Version Superseded: 27/10/2010
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There are currently no known outstanding effects for the Council Regulation (EC) No 423/2007 (repealed), Division
I.6
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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. |
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