10K+ items found
Search results
Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 μPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1 273 K (1 000 °C), and specially designed quartz heaters therefor. N.B.: SEE ALSO 9B106.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M15B4bCode: 9B006Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 μPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1 273 K (1 000 °C), and specially designed quartz heaters therefor. N.B.: SEE ALSO 9B106.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M15B4bCode: 9B006On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following: N.B.: SEE ALSO 9B105. a. Wind tunnels designed for speeds of Mach 1,2 or more; Note: 9B005.a. does not control wind tunnels specially designed for educational purposes and having a ‘test section size’ (measured laterally) of less than 250 mm. Technical Note: ‘Test section size’ means the diameter of the circle, or the side of the square, or the longest side of the rectangle, at the largest test section location. b. Devices for simulating flow-environments at speeds exceeding Mach 5, including hot-shot tunnels, plasma arc tunnels, shock tubes, shock tunnels, gas tunnels and light gas guns; or c. Wind tunnels or devices, other than two-dimensional sections, capable of simulating Reynolds number flows exceeding 25 × 10 6 .
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M15B2Code: 9B005On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following: N.B.: SEE ALSO 9B105. a. Wind tunnels designed for speeds of Mach 1,2 or more; Note: 9B005.a. does not control wind tunnels specially designed for educational purposes and having a ‘test section size’ (measured laterally) of less than 250 mm. Technical Note: ‘Test section size’ means the diameter of the circle, or the side of the square, or the longest side of the rectangle, at the largest test section location. b. Devices for simulating flow-environments at speeds exceeding Mach 5, including hot-shot tunnels, plasma arc tunnels, shock tubes, shock tunnels, gas tunnels and light gas guns; or c. Wind tunnels or devices, other than two-dimensional sections, capable of simulating Reynolds number flows exceeding 25 × 10 6 .
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M15B2Code: 9B005Umbilical and interstage electrical connectors specially designed for “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. Technical Note: Interstage connectors referred to in 9A121 also include electrical connectors installed between the “missile”, space launch vehicle or sounding rocket and their payload.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M11A5Code: 9A121Umbilical and interstage electrical connectors specially designed for “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. Technical Note: Interstage connectors referred to in 9A121 also include electrical connectors installed between the “missile”, space launch vehicle or sounding rocket and their payload.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M11A5Code: 9A121Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or ‘other liquid propellants’, used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A8Code: 9A120Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or ‘other liquid propellants’, used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A8Code: 9A120Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20A1aCode: 9A119Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20A1aCode: 9A119Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1aCode: 9A119Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1aCode: 9A119Devices to regulate combustion usable in engines, which are usable in “missiles” or unmanned aerial vehicles specified in 9A012 or 9A112.a., specified in 9A011 or 9A111.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A2Code: 9A118Devices to regulate combustion usable in engines, which are usable in “missiles” or unmanned aerial vehicles specified in 9A012 or 9A112.a., specified in 9A011 or 9A111.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A2Code: 9A118Staging mechanisms, separation mechanisms, and interstages, usable in “missiles”. N.B.: SEE ALSO 9A121.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A4Code: 9A117Staging mechanisms, separation mechanisms, and interstages, usable in “missiles”. N.B.: SEE ALSO 9A121.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A4Code: 9A117Reentry vehicles, usable in “missiles”, and equipment designed or modified therefor, as follows: a. Reentry vehicles; b. Heat shields and components therefor, fabricated of ceramic or ablative materials; c. Heat sinks and components therefor, fabricated of light-weight, high heat capacity materials; d. Electronic equipment specially designed for reentry vehicles.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1bCode: 9A116Reentry vehicles, usable in “missiles”, and equipment designed or modified therefor, as follows: a. Reentry vehicles; b. Heat shields and components therefor, fabricated of ceramic or ablative materials; c. Heat sinks and components therefor, fabricated of light-weight, high heat capacity materials; d. Electronic equipment specially designed for reentry vehicles.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1bCode: 9A116b. Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M12A2Code: 9A115b. Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M12A2Code: 9A115Launch support equipment as follows: a. Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or unmanned aerial vehicles specified in 9A012 or 9A112.a.;
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M12A1Code: 9A115Launch support equipment as follows: a. Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or unmanned aerial vehicles specified in 9A012 or 9A112.a.;
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M12A1Code: 9A115“Unmanned aerial vehicles” (“UAVs”), other than those specified in 9A012, as follows: a. “Unmanned aerial vehicles” (“UAVs”) capable of a range of 300 km; b. “Unmanned aerial vehicles” (“UAVs”) having all of the following: 1. Having any of the following: a. An autonomous flight control and navigation capability; or b. Capability of controlled flight out of the direct vision range involving a human operator; and 2. Having any of the following: a. Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or b. Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres. Technical Notes: 1. An aerosol consists of particulate or liquids other than fuel components, by products or additives, as part of the “payload” to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding. 2. An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M19A3Code: 9A112“Unmanned aerial vehicles” (“UAVs”), other than those specified in 9A012, as follows: a. “Unmanned aerial vehicles” (“UAVs”) capable of a range of 300 km; b. “Unmanned aerial vehicles” (“UAVs”) having all of the following: 1. Having any of the following: a. An autonomous flight control and navigation capability; or b. Capability of controlled flight out of the direct vision range involving a human operator; and 2. Having any of the following: a. Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or b. Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres. Technical Notes: 1. An aerosol consists of particulate or liquids other than fuel components, by products or additives, as part of the “payload” to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding. 2. An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M19A3Code: 9A112“Unmanned aerial vehicles” (“UAVs”), other than those specified in 9A012, as follows: a. “Unmanned aerial vehicles” (“UAVs”) capable of a range of 300 km; b. “Unmanned aerial vehicles” (“UAVs”) having all of the following: 1. Having any of the following: a. An autonomous flight control and navigation capability; or b. Capability of controlled flight out of the direct vision range involving a human operator; and 2. Having any of the following: a. Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or b. Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres. Technical Notes: 1. An aerosol consists of particulate or liquids other than fuel components, by products or additives, as part of the “payload” to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding. 2. An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M19A2Code: 9A112“Unmanned aerial vehicles” (“UAVs”), other than those specified in 9A012, as follows: a. “Unmanned aerial vehicles” (“UAVs”) capable of a range of 300 km; b. “Unmanned aerial vehicles” (“UAVs”) having all of the following: 1. Having any of the following: a. An autonomous flight control and navigation capability; or b. Capability of controlled flight out of the direct vision range involving a human operator; and 2. Having any of the following: a. Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or b. Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres. Technical Notes: 1. An aerosol consists of particulate or liquids other than fuel components, by products or additives, as part of the “payload” to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding. 2. An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M19A2Code: 9A112Pulse jet engines, usable in “missiles” or unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor. N.B.: SEE ALSO 9A011 AND 9A118.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A2Code: 9A111Pulse jet engines, usable in “missiles” or unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor. N.B.: SEE ALSO 9A011 AND 9A118.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A2Code: 9A111Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in ‘missiles’ or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119. N.B.: SEE ALSO 1A002. Technical Note: In 9A110 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M6A1Code: 9A110Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in ‘missiles’ or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119. N.B.: SEE ALSO 1A002. Technical Note: In 9A110 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M6A1Code: 9A110Hybrid rocket motors and specially designed components as follows: a. Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor; b. Specially designed components for hybrid rocket motors specified in 9A009 that are usable in “missiles”. N.B.: SEE ALSO 9A009 and 9A119.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1cCode: 9A109Hybrid rocket motors and specially designed components as follows: a. Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor; b. Specially designed components for hybrid rocket motors specified in 9A009 that are usable in “missiles”. N.B.: SEE ALSO 9A009 and 9A119.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1cCode: 9A109Hybrid rocket motors and specially designed components as follows: a. Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor; b. Specially designed components for hybrid rocket motors specified in 9A009 that are usable in “missiles”. N.B.: SEE ALSO 9A009 and 9A119.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20A1bCode: 9A109Hybrid rocket motors and specially designed components as follows: a. Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor; b. Specially designed components for hybrid rocket motors specified in 9A009 that are usable in “missiles”. N.B.: SEE ALSO 9A009 and 9A119.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20A1bCode: 9A109Hybrid rocket motors and specially designed components as follows: a. Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor; b. Specially designed components for hybrid rocket motors specified in 9A009 that are usable in “missiles”. N.B.: SEE ALSO 9A009 and 9A119.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A6Code: 9A109Hybrid rocket motors and specially designed components as follows: a. Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor; b. Specially designed components for hybrid rocket motors specified in 9A009 that are usable in “missiles”. N.B.: SEE ALSO 9A009 and 9A119.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A6Code: 9A109c. Thrust vector control sub-systems, usable in “missiles”. Technical Note: Examples of methods of achieving thrust vector control specified in 9A108.c. are: 1. Flexible nozzle; 2. Fluid or secondary gas injection; 3. Movable engine or nozzle; 4. Deflection of exhaust gas stream (jet vanes or probes); or 5. Thrust tabs.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1eCode: 9A108c. Thrust vector control sub-systems, usable in “missiles”. Technical Note: Examples of methods of achieving thrust vector control specified in 9A108.c. are: 1. Flexible nozzle; 2. Fluid or secondary gas injection; 3. Movable engine or nozzle; 4. Deflection of exhaust gas stream (jet vanes or probes); or 5. Thrust tabs.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2A1eCode: 9A108Components, other than those specified in 9A008, as follows, specially designed for solid rocket propulsion systems: a. Rocket motor cases and “insulation” components therefor, usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; b. Rocket nozzles, usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A3Code: 9A108Components, other than those specified in 9A008, as follows, specially designed for solid rocket propulsion systems: a. Rocket motor cases and “insulation” components therefor, usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; b. Rocket nozzles, usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3A3Code: 9A108