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  • Good

    Space launch vehicles, ‘spacecraft’, ‘spacecraft buses’, ‘spacecraft payloads’, ‘spacecraft’ on-board systems or equipment, and terrestrial equipment, as follows: (a) Space launch vehicles; (b) ‘Spacecraft’; (c) ‘Spacecraft buses’; (d) ‘Spacecraft payloads’ incorporating items specified in this list; (e) On-board systems or equipment, specially designed for ‘spacecraft’ and having any of the following functions: 1. ‘Command and telemetry data handling’; (f) Terrestrial equipment specially designed for ‘spacecraft’, as follows: 1. Telemetry and telecommand equipment; 2. Simulators.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.004
    Code: 9A004
    Good

    Space launch vehicles, ‘spacecraft’, ‘spacecraft buses’, ‘spacecraft payloads’, ‘spacecraft’ on-board systems or equipment, and terrestrial equipment, as follows: (a) Space launch vehicles; (b) ‘Spacecraft’; (c) ‘Spacecraft buses’; (d) ‘Spacecraft payloads’ incorporating items specified in this list; (e) On-board systems or equipment, specially designed for ‘spacecraft’ and having any of the following functions: 1. ‘Command and telemetry data handling’; (f) Terrestrial equipment specially designed for ‘spacecraft’, as follows: 1. Telemetry and telecommand equipment; 2. Simulators.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.004
    Code: 9A004
  • Good

    Specially designed assemblies or components, incorporating any of the ‘technologies’ specified in paragraph 2 of the section below entitled ‘Technology’, for any of the following aero gas turbine engines: (a) Specified in item 1 above; or (b) Whose design or production origins are unknown to the manufacturer.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.003
    Code: 9A003
    Good

    Specially designed assemblies or components, incorporating any of the ‘technologies’ specified in paragraph 2 of the section below entitled ‘Technology’, for any of the following aero gas turbine engines: (a) Specified in item 1 above; or (b) Whose design or production origins are unknown to the manufacturer.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.003
    Code: 9A003
  • Good

    ‘Marine gas turbine engines’ with an ISO standard continuous power rating of 24 245 kW or more and a specific fuel consumption not exceeding 0,219 kg/kWh in the power range from 35 to 100 %, and specially designed assemblies and components therefor. Note : The term ‘marine gas turbine engines’ includes those industrial, or aero-derivative, gas turbine engines adapted for a ship's electric power generation or propulsion.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.002
    Code: 9A002
    Good

    ‘Marine gas turbine engines’ with an ISO standard continuous power rating of 24 245 kW or more and a specific fuel consumption not exceeding 0,219 kg/kWh in the power range from 35 to 100 %, and specially designed assemblies and components therefor. Note : The term ‘marine gas turbine engines’ includes those industrial, or aero-derivative, gas turbine engines adapted for a ship's electric power generation or propulsion.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.002
    Code: 9A002
  • Good

    Aero gas turbine engines: (a) Incorporating any of the ‘technologies’ specified in paragraph 2 of the section below entitled ‘Technology’; or Note 1 : This item does not apply to aero gas turbine engines which meet all of the following: (a) Certified by civil aviation authorities; and (b) Intended to power non-military manned ‘aircraft’ for which any of the following has been issued by civil aviation authorities for the ‘aircraft’ with this specific engine type: 1. A civil type certificate; or 2. An equivalent document recognized by ICAO. Note 2 : This item does not apply to aero gas turbine engines designed for Auxiliary Power Units (APUs) approved by the civil aviation authority of the Member State. (b) Designed to power an ‘aircraft’ designed to cruise at Mach 1 or higher, for more than 30 minutes.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.001
    Code: 9A001
    Good

    Aero gas turbine engines: (a) Incorporating any of the ‘technologies’ specified in paragraph 2 of the section below entitled ‘Technology’; or Note 1 : This item does not apply to aero gas turbine engines which meet all of the following: (a) Certified by civil aviation authorities; and (b) Intended to power non-military manned ‘aircraft’ for which any of the following has been issued by civil aviation authorities for the ‘aircraft’ with this specific engine type: 1. A civil type certificate; or 2. An equivalent document recognized by ICAO. Note 2 : This item does not apply to aero gas turbine engines designed for Auxiliary Power Units (APUs) approved by the civil aviation authority of the Member State. (b) Designed to power an ‘aircraft’ designed to cruise at Mach 1 or higher, for more than 30 minutes.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A9.001
    Code: 9A001
  • Good

    Equipment specially designed for the ‘production’ of equipment specified IN IX.A7. Note : Including: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre-optic gyro coil winding machines.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.006
    Code: 7B003
    Good

    Equipment specially designed for the ‘production’ of equipment specified IN IX.A7. Note : Including: — Gyro tuning test stations; — Gyro dynamic balance stations; — Gyro run-in/motor test stations; — Gyro evacuation and fill stations; — Centrifuge fixtures for gyro bearings; — Accelerometer axis align stations; — Fibre-optic gyro coil winding machines.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.006
    Code: 7B003
  • Good

    Equipment specially designed to characterize mirrors for ring ‘laser’ gyros, as follows: (a) Scatterometers having a measurement ‘accuracy’ of 10 ppm or less (better); (b) Profilometers having a measurement ‘accuracy’ of 0,5 nm (5 angstrom) or less (better).

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.005
    Code: 7B002
    Good

    Equipment specially designed to characterize mirrors for ring ‘laser’ gyros, as follows: (a) Scatterometers having a measurement ‘accuracy’ of 10 ppm or less (better); (b) Profilometers having a measurement ‘accuracy’ of 0,5 nm (5 angstrom) or less (better).

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.005
    Code: 7B002
  • Good

    Test, calibration or alignment equipment, specially designed for equipment specified in the section above.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.004
    Code: 7B001
    Good

    Test, calibration or alignment equipment, specially designed for equipment specified in the section above.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.004
    Code: 7B001
  • Good

    Airborne altimeters operating at frequencies other than 4,2 to 4,4 GHz inclusive and having any of the following: (a) ‘Power management’; or (b) Using phase shift key modulation.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.003
    Code: 7A006
    Good

    Airborne altimeters operating at frequencies other than 4,2 to 4,4 GHz inclusive and having any of the following: (a) ‘Power management’; or (b) Using phase shift key modulation.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.003
    Code: 7A006
  • Good

    Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following and specially designed components therefor: (a) Employing a decryption algorithm specially designed or modified for government use to access the ranging code for position and time; or (b) Employing ‘adaptive antenna systems’. Note : Item (b) does not apply to GNSS receiving equipment that only uses components designed to filter, switch or combine signals from multiple omni-directional antennae that do not implement adaptive antenna techniques. Technical note: For the purposes of item (b), ‘adaptive antenna systems’ dynamically generate one or more spatial nulls in an antenna array pattern by signal processing in the time domain or frequency domain.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.002
    Code: 7A005
    Good

    Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following and specially designed components therefor: (a) Employing a decryption algorithm specially designed or modified for government use to access the ranging code for position and time; or (b) Employing ‘adaptive antenna systems’. Note : Item (b) does not apply to GNSS receiving equipment that only uses components designed to filter, switch or combine signals from multiple omni-directional antennae that do not implement adaptive antenna techniques. Technical note: For the purposes of item (b), ‘adaptive antenna systems’ dynamically generate one or more spatial nulls in an antenna array pattern by signal processing in the time domain or frequency domain.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.002
    Code: 7A005
  • Good

    ‘Star trackers’ and components therefor, as follows: (a) ‘Star trackers’ with a specified azimuth ‘accuracy’ of equal to or less (better) than 20 seconds of arc throughout the specified lifetime of the equipment; (b) Components specially designed for equipment specified in item (a), as follows: 1. Optical heads or baffles; 2. Data processing units. Technical note: ‘Star trackers’ are also referred to as stellar attitude sensors or gyro-astro compasses.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.001
    Code: 7A004
    Good

    ‘Star trackers’ and components therefor, as follows: (a) ‘Star trackers’ with a specified azimuth ‘accuracy’ of equal to or less (better) than 20 seconds of arc throughout the specified lifetime of the equipment; (b) Components specially designed for equipment specified in item (a), as follows: 1. Optical heads or baffles; 2. Data processing units. Technical note: ‘Star trackers’ are also referred to as stellar attitude sensors or gyro-astro compasses.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A7.001
    Code: 7A004
  • Good

    ‘Laser’ materials, as follows: (a) Synthetic crystalline ‘laser’ host material in unfinished form as follows: 1. Titanium doped sapphire; (b) Rare-earth-metal doped double-clad fibres; 1. Nominal ‘laser’ wavelength of 975 nm to 1 150 nm and having all of the following: a. Average core diameter equal to or greater than 25 μm; and b. Core ‘Numerical Aperture’ (‘NA’) less than 0,065; or Note : The item above does not apply to double-clad fibres having an inner glass cladding diameter exceeding 150 μm and not exceeding 300 μm. 2. Nominal ‘laser’ wavelength exceeding 1 530 nm and having all of the following: a. Average core diameter equal to or greater than 20 μm; and b. Core ‘NA’ less than 0,1. Technical notes: 1. For the purposes of the item above, the core ‘Numerical Aperture’ (‘NA’) is measured at the emission wavelengths of the fibre. 2. Item (b) above includes fibres assembled with end caps.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.027
    Code: 6C005
    Good

    ‘Laser’ materials, as follows: (a) Synthetic crystalline ‘laser’ host material in unfinished form as follows: 1. Titanium doped sapphire; (b) Rare-earth-metal doped double-clad fibres; 1. Nominal ‘laser’ wavelength of 975 nm to 1 150 nm and having all of the following: a. Average core diameter equal to or greater than 25 μm; and b. Core ‘Numerical Aperture’ (‘NA’) less than 0,065; or Note : The item above does not apply to double-clad fibres having an inner glass cladding diameter exceeding 150 μm and not exceeding 300 μm. 2. Nominal ‘laser’ wavelength exceeding 1 530 nm and having all of the following: a. Average core diameter equal to or greater than 20 μm; and b. Core ‘NA’ less than 0,1. Technical notes: 1. For the purposes of the item above, the core ‘Numerical Aperture’ (‘NA’) is measured at the emission wavelengths of the fibre. 2. Item (b) above includes fibres assembled with end caps.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.027
    Code: 6C005
  • Good

    Optical sensor materials, as follows: (a) Elemental tellurium (Te) of purity levels of 99,9995 % or more; (b) Single crystals (including epitaxial wafers) of any of the following: 1. Cadmium zinc telluride (CdZnTe) with zinc content of less than 6 % by ‘mole fraction’; 2. Cadmium telluride (CdTe) of any purity level; or 3. Mercury cadmium telluride (HgCdTe) of any purity level. Technical note: ‘Mole fraction’ is defined as the ratio of moles of ZnTe to the sum of the moles of CdTe and ZnTe present in the crystal.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.023
    Code: 6C002
    Good

    Optical sensor materials, as follows: (a) Elemental tellurium (Te) of purity levels of 99,9995 % or more; (b) Single crystals (including epitaxial wafers) of any of the following: 1. Cadmium zinc telluride (CdZnTe) with zinc content of less than 6 % by ‘mole fraction’; 2. Cadmium telluride (CdTe) of any purity level; or 3. Mercury cadmium telluride (HgCdTe) of any purity level. Technical note: ‘Mole fraction’ is defined as the ratio of moles of ZnTe to the sum of the moles of CdTe and ZnTe present in the crystal.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.023
    Code: 6C002
  • Good

    Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.022
    Code: 6B008
    Good

    Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.022
    Code: 6B008
  • Good

    Equipment to produce, align and calibrate land-based gravity meters with a static ‘accuracy’ of better than 0,1 mGal.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.021
    Code: 6B007
    Good

    Equipment to produce, align and calibrate land-based gravity meters with a static ‘accuracy’ of better than 0,1 mGal.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.021
    Code: 6B007
  • Good

    Optical equipment, as follows: (a) Equipment for measuring absolute reflectance to an ‘accuracy’ of equal to or better than 0,1 % of the reflectance value; (b) Equipment other than optical surface scattering measurement equipment, having an unobscured aperture of more than 10 cm, specially designed for the non-contact optical measurement of a non-planar optical surface figure (profile) to an ‘accuracy’ of 2 nm or less (better) against the required profile. Note : The item above does not apply to microscopes.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.020
    Code: 6B004
    Good

    Optical equipment, as follows: (a) Equipment for measuring absolute reflectance to an ‘accuracy’ of equal to or better than 0,1 % of the reflectance value; (b) Equipment other than optical surface scattering measurement equipment, having an unobscured aperture of more than 10 cm, specially designed for the non-contact optical measurement of a non-planar optical surface figure (profile) to an ‘accuracy’ of 2 nm or less (better) against the required profile. Note : The item above does not apply to microscopes.

    Authority: EU
    Prohibited Supply To: KP
    Program: KP
    EU Code: IX.A6.020
    Code: 6B004
  • Good

    1. Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor: Note : This section does not apply to: — Secondary Surveillance Radar (SSR); — Civil Automotive Radar; — Displays or monitors used for Air Traffic Control (ATC); — Meteorological (weather) Radar; — Precision Approach Radar (PAR) equipment conforming to International Civil Aviation Organization (ICAO) standards and employing electronically steerable linear (one-dimensional) arrays or mechanically positioned passive antennae. (a) Operating at frequencies from 40 GHz to 230 GHz and having any of the following: 1. An average output power exceeding 100 mW; or 2. Locating ‘accuracy’ of 1 m or less (better) in range and 0,2 degree or less (better) in azimuth; (b) A tunable bandwidth exceeding ± 6,25 % of the ‘centre operating frequency’; Technical note: The ‘centre operating frequency’ equals one half of the sum of the highest plus the lowest specified operating frequencies. (c) Capable of operating simultaneously on more than two carrier frequencies; (d) Capable of operating in synthetic aperture radar (SAR), inverse synthetic aperture radar (ISAR) or side-looking airborne radar (SLAR) mode; (e) Incorporating electronically steerable array antennae; (f) Capable of height-finding non-cooperative targets; (g) Specially designed for airborne (balloon or airframe mounted) operation and having Doppler ‘signal processing’ for the detection of moving targets; (h) Employing processing of radar signals and using any of the following: 1. ‘Radar spread spectrum’ techniques; or 2. ‘Radar frequency agility’ techniques; (i) Providing ground-based operation with a maximum ‘instrumented range’ exceeding 185 km; Note : Item (i) above does not apply to: (a) Fishing ground surveillance radar; (b) Ground radar equipment specially designed for en-route air traffic control and having all of the following: 1. A maximum ‘instrumented range’ of 500 km or less; 2. Configured so that radar target data can be transmitted only one way from the radar site to one or more civil ATC centres; 3. Contains no provisions for remote control of the radar scan rate from the en-route ATC centre; and 4. Permanently installed. (c) Weather balloon tracking radars. (j) Being ‘laser’ radar or Light Detection and Ranging (LIDAR) equipment and having any of the following: 1. ‘Space-qualified’; 2. Employing coherent heterodyne or homodyne detection techniques and having an angular resolution of less (better) than 20 μrad (microradians); or 3. Designed for carrying out airborne bathymetric littoral surveys to International Hydrographic Organization (IHO) Order 1a Standard (5th Edition, February 2008) for Hydrographic Surveys or better, and using one or more ‘lasers’ with a wavelength exceeding 400 nm but not exceeding 600 nm; Notes: 1. LIDAR equipment specially designed for surveying is only specified by 3. 2. The item above does not apply to LIDAR equipment specially designed for meteorological observation. 3. Parameters in the IHO Order 1a Standard (5th Edition, February 2008) are summarized as follows: Horizontal Accuracy (95 % confidence level) = 5 m + 5 % of depth. Depth Accuracy for Reduced Depths (95 % confidence level) = ± √(a 2 + (b * d) 2 ) where: a = 0,5 m = constant-depth error, i.e., the sum of all constant-depth errors b = 0,013 = factor of depth-dependent error b * d = depth-dependent error, i.e., the sum of all depth-dependent errors d = depth Feature Detection = Cubic features > 2 m in depths up to 40 m; 10 % of depth beyond 40 m. (k) Having ‘signal processing’ subsystems using ‘pulse compression’ and having any of the following: 1. A ‘pulse compression’ ratio exceeding 150; or 2. A compressed pulse width of less than 200 ns; or Note : Item 2. above does not apply to two-dimensional ‘marine radar’ or ‘vessel traffic service’ radar, having all of the following: (a) ‘Pulse compression’ ratio not exceeding 150; (b) Compressed pulse width of greater than 30 ns; (c) Single and rotating mechanically scanned antenna; (d) Peak output power not exceeding 250 W; and (e) Not capable of ‘frequency hopping’. (l) Having data processing subsystems and having any of the following: 1. ‘Automatic target tracking’ providing, at any antenna rotation, the predicted target position beyond the time of the next antenna beam passage; or Note : The item above does not apply to conflict alert capability in ATC systems, or ‘marine radar’. 2. Configured to provide superposition and correlation, or fusion, of target data within six seconds from two or more ‘geographically dispersed’ radar sensors to improve the aggregate performance beyond that of any single sensor specified in items (f) or (i). Note : The item above does not apply to systems, equipment and assemblies used for ‘vessel traffic services’. Technical notes: 1. For the purposes of this section, ‘marine radar’ is a radar that is used to navigate safely at sea, in inland waterways or in near-shore environments. 2. For the purposes of this section, ‘vessel traffic service’ is a vessel traffic monitoring and control service similar to air traffic control for ‘aircraft’.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.019
    Code: 6A008
    Good

    1. Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor: Note : This section does not apply to: — Secondary Surveillance Radar (SSR); — Civil Automotive Radar; — Displays or monitors used for Air Traffic Control (ATC); — Meteorological (weather) Radar; — Precision Approach Radar (PAR) equipment conforming to International Civil Aviation Organization (ICAO) standards and employing electronically steerable linear (one-dimensional) arrays or mechanically positioned passive antennae. (a) Operating at frequencies from 40 GHz to 230 GHz and having any of the following: 1. An average output power exceeding 100 mW; or 2. Locating ‘accuracy’ of 1 m or less (better) in range and 0,2 degree or less (better) in azimuth; (b) A tunable bandwidth exceeding ± 6,25 % of the ‘centre operating frequency’; Technical note: The ‘centre operating frequency’ equals one half of the sum of the highest plus the lowest specified operating frequencies. (c) Capable of operating simultaneously on more than two carrier frequencies; (d) Capable of operating in synthetic aperture radar (SAR), inverse synthetic aperture radar (ISAR) or side-looking airborne radar (SLAR) mode; (e) Incorporating electronically steerable array antennae; (f) Capable of height-finding non-cooperative targets; (g) Specially designed for airborne (balloon or airframe mounted) operation and having Doppler ‘signal processing’ for the detection of moving targets; (h) Employing processing of radar signals and using any of the following: 1. ‘Radar spread spectrum’ techniques; or 2. ‘Radar frequency agility’ techniques; (i) Providing ground-based operation with a maximum ‘instrumented range’ exceeding 185 km; Note : Item (i) above does not apply to: (a) Fishing ground surveillance radar; (b) Ground radar equipment specially designed for en-route air traffic control and having all of the following: 1. A maximum ‘instrumented range’ of 500 km or less; 2. Configured so that radar target data can be transmitted only one way from the radar site to one or more civil ATC centres; 3. Contains no provisions for remote control of the radar scan rate from the en-route ATC centre; and 4. Permanently installed. (c) Weather balloon tracking radars. (j) Being ‘laser’ radar or Light Detection and Ranging (LIDAR) equipment and having any of the following: 1. ‘Space-qualified’; 2. Employing coherent heterodyne or homodyne detection techniques and having an angular resolution of less (better) than 20 μrad (microradians); or 3. Designed for carrying out airborne bathymetric littoral surveys to International Hydrographic Organization (IHO) Order 1a Standard (5th Edition, February 2008) for Hydrographic Surveys or better, and using one or more ‘lasers’ with a wavelength exceeding 400 nm but not exceeding 600 nm; Notes: 1. LIDAR equipment specially designed for surveying is only specified by 3. 2. The item above does not apply to LIDAR equipment specially designed for meteorological observation. 3. Parameters in the IHO Order 1a Standard (5th Edition, February 2008) are summarized as follows: Horizontal Accuracy (95 % confidence level) = 5 m + 5 % of depth. Depth Accuracy for Reduced Depths (95 % confidence level) = ± √(a 2 + (b * d) 2 ) where: a = 0,5 m = constant-depth error, i.e., the sum of all constant-depth errors b = 0,013 = factor of depth-dependent error b * d = depth-dependent error, i.e., the sum of all depth-dependent errors d = depth Feature Detection = Cubic features > 2 m in depths up to 40 m; 10 % of depth beyond 40 m. (k) Having ‘signal processing’ subsystems using ‘pulse compression’ and having any of the following: 1. A ‘pulse compression’ ratio exceeding 150; or 2. A compressed pulse width of less than 200 ns; or Note : Item 2. above does not apply to two-dimensional ‘marine radar’ or ‘vessel traffic service’ radar, having all of the following: (a) ‘Pulse compression’ ratio not exceeding 150; (b) Compressed pulse width of greater than 30 ns; (c) Single and rotating mechanically scanned antenna; (d) Peak output power not exceeding 250 W; and (e) Not capable of ‘frequency hopping’. (l) Having data processing subsystems and having any of the following: 1. ‘Automatic target tracking’ providing, at any antenna rotation, the predicted target position beyond the time of the next antenna beam passage; or Note : The item above does not apply to conflict alert capability in ATC systems, or ‘marine radar’. 2. Configured to provide superposition and correlation, or fusion, of target data within six seconds from two or more ‘geographically dispersed’ radar sensors to improve the aggregate performance beyond that of any single sensor specified in items (f) or (i). Note : The item above does not apply to systems, equipment and assemblies used for ‘vessel traffic services’. Technical notes: 1. For the purposes of this section, ‘marine radar’ is a radar that is used to navigate safely at sea, in inland waterways or in near-shore environments. 2. For the purposes of this section, ‘vessel traffic service’ is a vessel traffic monitoring and control service similar to air traffic control for ‘aircraft’.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.019
    Code: 6A008
  • Good

    Gravity meters (gravimeters) and gravity gradiometers, as follows: (a) Gravity meters designed or modified for ground use and having a static ‘accuracy’ of less (better) than 10 μGal; Note : Item (a) does not apply to ground gravity meters of the quartz element (Worden) type. (b) Gravity meters designed for mobile platforms and having all of the following: 1. A static ‘accuracy’ of less (better) than 0,7 mGal; and 2. An in-service (operational) ‘accuracy’ of less (better) than 0,7 mGal having a ‘time-to-steady-state registration’ of less than 2 minutes under any combination of attendant corrective compensations and motional influences; Technical note : For the purposes of item (b), ‘time-to-steady-state registration’ (also referred to as the gravimeter's response time) is the time over which the disturbing effects of platform-induced accelerations (high-frequency noise) are reduced. (c) Gravity gradiometers.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.018
    Code: 6A007
    Good

    Gravity meters (gravimeters) and gravity gradiometers, as follows: (a) Gravity meters designed or modified for ground use and having a static ‘accuracy’ of less (better) than 10 μGal; Note : Item (a) does not apply to ground gravity meters of the quartz element (Worden) type. (b) Gravity meters designed for mobile platforms and having all of the following: 1. A static ‘accuracy’ of less (better) than 0,7 mGal; and 2. An in-service (operational) ‘accuracy’ of less (better) than 0,7 mGal having a ‘time-to-steady-state registration’ of less than 2 minutes under any combination of attendant corrective compensations and motional influences; Technical note : For the purposes of item (b), ‘time-to-steady-state registration’ (also referred to as the gravimeter's response time) is the time over which the disturbing effects of platform-induced accelerations (high-frequency noise) are reduced. (c) Gravity gradiometers.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.018
    Code: 6A007
  • Good

    Imaging cameras incorporating ‘focal plane arrays’ having any of the following: a. Incorporating non-‘space-qualified’‘focal plane arrays’ having any of the following: 1. Having all of the following: a. Individual elements with a peak response within the wavelength range exceeding 900 nm but not exceeding 1 050 nm; and b. Any of the following: 1. A response ‘time constant’ of less than 0,5 ns; or 2. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum ‘radiant sensitivity’ exceeding 10 mA/W; 2. Having all of the following: a. Individual elements with a peak response in the wavelength range exceeding 1 050 nm but not exceeding 1 200 nm; and b. Any of the following: 1. A response ‘time constant’ of 95 ns or less; or 2. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum ‘radiant sensitivity’ exceeding 10 mA/W; or 3. Being non-‘space-qualified’ non-linear (two-dimensional) ‘focal plane arrays’ having individual elements with a peak response in the wavelength range exceeding 1 200 nm but not exceeding 30 000 nm; 4. Being non-‘space-qualified’ linear (one-dimensional) ‘focal plane arrays’ having all of the following: a. Individual elements with a peak response in the wavelength range exceeding 1 200 nm but not exceeding 3 000 nm; and b. Any of the following: 1. A ratio of ‘scan direction’ dimension of the detector element to the ‘cross-scan direction’ dimension of the detector element of less than 3,8; or 2. Signal processing in the detector elements; or 5. Being non-‘space-qualified’ linear (one-dimensional) ‘focal plane arrays’ having individual elements with a peak response in the wavelength range exceeding 3 000 nm but not exceeding 30 000 nm; b. Incorporating non-‘space-qualified’ non-linear (two-dimensional) infrared ‘focal plane arrays’ based on ‘microbolometer’ material having individual elements with an unfiltered response in the wavelength range equal to or exceeding 8 000 nm but not exceeding 14 000 nm; or c. Incorporating non-‘space-qualified’‘focal plane arrays’ having all of the following: 1. Individual detector elements with a peak response in the wavelength range exceeding 400 nm but not exceeding 900 nm; 2. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum ‘radiant sensitivity’ exceeding 10 mA/W for wavelengths exceeding 760 nm; and 3. Greater than 32 elements. Notes: 1. Imaging cameras specified in item 4 above include ‘focal plane arrays’ combined with sufficient ‘signal processing’ electronics, beyond the read-out integrated circuit, to enable as a minimum the output of an analogue or digital signal once power is supplied. 2. Item 4.a. does not apply to imaging cameras incorporating linear ‘focal plane arrays’ with 12 elements or fewer, not employing time-delay-and-integration within the element and designed for any of the following: (a) Industrial or civilian intrusion alarm, traffic or industrial movement control or counting systems; (b) Industrial equipment used for inspection or monitoring of heat flows in buildings, equipment or industrial processes; (c) Industrial equipment used for inspection, sorting or analysis of the properties of materials; (d) Equipment specially designed for laboratory use; or (e) Medical equipment. 3. Item 4.b. does not apply to imaging cameras having any of the following: (a) A maximum frame rate equal to or less than 9 Hz; (b) Having all of the following: 1. Having a minimum horizontal or vertical ‘Instantaneous Field of View (IFOV)’ of at least 10 mrad (milliradians); 2. Incorporating a fixed focal-length lens that is not designed to be removed; 3. Not incorporating a ‘direct view’ display; and Technical note: ‘Direct view’ refers to an imaging camera operating in the infrared spectrum that presents a visual image to a human observer using a near-to-eye microdisplay incorporating any light-security mechanism. 4. Having any of the following: a. No facility to obtain a viewable image of the detected field of view; or b. The camera is designed for a single kind of application and designed not to be user modified; or Technical note: ‘Instantaneous Field of View (IFOV)’ specified in note 3.b. is the lesser figure of the ‘Horizontal IFOV’ or the ‘Vertical IFOV’. ‘Horizontal IFOV’ = horizontal Field of View (FOV)/number of horizontal detector elements. ‘Vertical IFOV’ = vertical Field of View (FOV)/number of vertical detector elements. (c) The camera is specially designed for installation into a civilian passenger land vehicle and having all of the following: 1. The placement and configuration of the camera within the vehicle are solely to assist the driver in the safe operation of the vehicle.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.009
    Code: 6A003
    Good

    Imaging cameras incorporating ‘focal plane arrays’ having any of the following: a. Incorporating non-‘space-qualified’‘focal plane arrays’ having any of the following: 1. Having all of the following: a. Individual elements with a peak response within the wavelength range exceeding 900 nm but not exceeding 1 050 nm; and b. Any of the following: 1. A response ‘time constant’ of less than 0,5 ns; or 2. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum ‘radiant sensitivity’ exceeding 10 mA/W; 2. Having all of the following: a. Individual elements with a peak response in the wavelength range exceeding 1 050 nm but not exceeding 1 200 nm; and b. Any of the following: 1. A response ‘time constant’ of 95 ns or less; or 2. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum ‘radiant sensitivity’ exceeding 10 mA/W; or 3. Being non-‘space-qualified’ non-linear (two-dimensional) ‘focal plane arrays’ having individual elements with a peak response in the wavelength range exceeding 1 200 nm but not exceeding 30 000 nm; 4. Being non-‘space-qualified’ linear (one-dimensional) ‘focal plane arrays’ having all of the following: a. Individual elements with a peak response in the wavelength range exceeding 1 200 nm but not exceeding 3 000 nm; and b. Any of the following: 1. A ratio of ‘scan direction’ dimension of the detector element to the ‘cross-scan direction’ dimension of the detector element of less than 3,8; or 2. Signal processing in the detector elements; or 5. Being non-‘space-qualified’ linear (one-dimensional) ‘focal plane arrays’ having individual elements with a peak response in the wavelength range exceeding 3 000 nm but not exceeding 30 000 nm; b. Incorporating non-‘space-qualified’ non-linear (two-dimensional) infrared ‘focal plane arrays’ based on ‘microbolometer’ material having individual elements with an unfiltered response in the wavelength range equal to or exceeding 8 000 nm but not exceeding 14 000 nm; or c. Incorporating non-‘space-qualified’‘focal plane arrays’ having all of the following: 1. Individual detector elements with a peak response in the wavelength range exceeding 400 nm but not exceeding 900 nm; 2. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum ‘radiant sensitivity’ exceeding 10 mA/W for wavelengths exceeding 760 nm; and 3. Greater than 32 elements. Notes: 1. Imaging cameras specified in item 4 above include ‘focal plane arrays’ combined with sufficient ‘signal processing’ electronics, beyond the read-out integrated circuit, to enable as a minimum the output of an analogue or digital signal once power is supplied. 2. Item 4.a. does not apply to imaging cameras incorporating linear ‘focal plane arrays’ with 12 elements or fewer, not employing time-delay-and-integration within the element and designed for any of the following: (a) Industrial or civilian intrusion alarm, traffic or industrial movement control or counting systems; (b) Industrial equipment used for inspection or monitoring of heat flows in buildings, equipment or industrial processes; (c) Industrial equipment used for inspection, sorting or analysis of the properties of materials; (d) Equipment specially designed for laboratory use; or (e) Medical equipment. 3. Item 4.b. does not apply to imaging cameras having any of the following: (a) A maximum frame rate equal to or less than 9 Hz; (b) Having all of the following: 1. Having a minimum horizontal or vertical ‘Instantaneous Field of View (IFOV)’ of at least 10 mrad (milliradians); 2. Incorporating a fixed focal-length lens that is not designed to be removed; 3. Not incorporating a ‘direct view’ display; and Technical note: ‘Direct view’ refers to an imaging camera operating in the infrared spectrum that presents a visual image to a human observer using a near-to-eye microdisplay incorporating any light-security mechanism. 4. Having any of the following: a. No facility to obtain a viewable image of the detected field of view; or b. The camera is designed for a single kind of application and designed not to be user modified; or Technical note: ‘Instantaneous Field of View (IFOV)’ specified in note 3.b. is the lesser figure of the ‘Horizontal IFOV’ or the ‘Vertical IFOV’. ‘Horizontal IFOV’ = horizontal Field of View (FOV)/number of horizontal detector elements. ‘Vertical IFOV’ = vertical Field of View (FOV)/number of vertical detector elements. (c) The camera is specially designed for installation into a civilian passenger land vehicle and having all of the following: 1. The placement and configuration of the camera within the vehicle are solely to assist the driver in the safe operation of the vehicle.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.009
    Code: 6A003
  • Good

    Imaging cameras incorporating image intensifier tubes having any of the following: a. Having all of the following: 1. A peak response in the wavelength range exceeding 400 nm but not exceeding 1 050 nm; 2. Electron image amplification using any of the following: a. A microchannel plate with a hole pitch (centre-to-centre spacing) of 12 μm or less; or b. An electron sensing device with a non-binned pixel pitch of 500 μm or less, specially designed or modified to achieve ‘charge multiplication’ other than by a microchannel plate; and 3. Any of the following photocathodes: a. Multialkali photocathodes (e.g., S-20 and S-25) having a luminous sensitivity exceeding 350 μA/lm; b. GaAs or GaInAs photocathodes; or c. Other ‘III/V compound’ semiconductor photocathodes having a maximum ‘radiant sensitivity’ exceeding 10 mA/W; or b. Having all of the following: 1. A peak response in the wavelength range exceeding 1 050 nm but not exceeding 1 800 nm; 2. Electron image amplification using any of the following: a. A microchannel plate with a hole pitch (centre-to-centre spacing) of 12 μm or less; or b. An electron sensing device with a non-binned pixel pitch of 500 μm or less, specially designed or modified to achieve ‘charge multiplication’ other than by a microchannel plate; and 3. ‘III/V compound’ semiconductor (e.g., GaAs or GaInAs) photocathodes and transferred electron photocathodes, having a maximum ‘radiant sensitivity’ exceeding 15 mA/W;

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.008
    Code: 6A003
    Good

    Imaging cameras incorporating image intensifier tubes having any of the following: a. Having all of the following: 1. A peak response in the wavelength range exceeding 400 nm but not exceeding 1 050 nm; 2. Electron image amplification using any of the following: a. A microchannel plate with a hole pitch (centre-to-centre spacing) of 12 μm or less; or b. An electron sensing device with a non-binned pixel pitch of 500 μm or less, specially designed or modified to achieve ‘charge multiplication’ other than by a microchannel plate; and 3. Any of the following photocathodes: a. Multialkali photocathodes (e.g., S-20 and S-25) having a luminous sensitivity exceeding 350 μA/lm; b. GaAs or GaInAs photocathodes; or c. Other ‘III/V compound’ semiconductor photocathodes having a maximum ‘radiant sensitivity’ exceeding 10 mA/W; or b. Having all of the following: 1. A peak response in the wavelength range exceeding 1 050 nm but not exceeding 1 800 nm; 2. Electron image amplification using any of the following: a. A microchannel plate with a hole pitch (centre-to-centre spacing) of 12 μm or less; or b. An electron sensing device with a non-binned pixel pitch of 500 μm or less, specially designed or modified to achieve ‘charge multiplication’ other than by a microchannel plate; and 3. ‘III/V compound’ semiconductor (e.g., GaAs or GaInAs) photocathodes and transferred electron photocathodes, having a maximum ‘radiant sensitivity’ exceeding 15 mA/W;

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.008
    Code: 6A003
  • Good

    Scanning cameras and scanning camera systems; a. A peak response in the wavelength range exceeding 10 nm, but not exceeding 30 000 nm; b. Linear detector arrays with more than 8 192 elements per array; and c. Mechanical scanning in one direction; Note : The item above does not apply to scanning cameras and scanning camera systems, specially designed for any of the following: (a) Industrial or civilian photocopiers; (b) Image scanners specially designed for civil, stationary, close proximity scanning applications (e.g., reproduction of images or print contained in documents, artwork or photographs); or (c) Medical equipment.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.007
    Code: 6A003
    Good

    Scanning cameras and scanning camera systems; a. A peak response in the wavelength range exceeding 10 nm, but not exceeding 30 000 nm; b. Linear detector arrays with more than 8 192 elements per array; and c. Mechanical scanning in one direction; Note : The item above does not apply to scanning cameras and scanning camera systems, specially designed for any of the following: (a) Industrial or civilian photocopiers; (b) Image scanners specially designed for civil, stationary, close proximity scanning applications (e.g., reproduction of images or print contained in documents, artwork or photographs); or (c) Medical equipment.

    Authority: EU
    Prohibited Supply To: IRKP
    Program: KP
    EU Code: IX.A6.007
    Code: 6A003
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