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“Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M3D1Code: 9D101“Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M3D1Code: 9D101“Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2D1Code: 9D101“Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2D1Code: 9D101“Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M1D1Code: 9D101“Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M1D1Code: 9D101Other “software” as follows: a. 2D or 3D viscous “software”, validated with wind tunnel or flight test data required for detailed engine flow modelling; b. “Software” for testing aero gas turbine engines, assemblies or components, specially designed to collect, reduce and analyse data in real time and capable of feedback control, including the dynamic adjustment of test articles or test conditions, as the test is in progress; c. “Software” specially designed to control directional solidification or single-crystal material growth in equipment specified in 9B001.a. or 9B001.c.; d. Not used; e. “Software” specially designed or modified for the operation of items specified in 9A012; f. “Software” specially designed to design the internal cooling passages of aero gas turbine blades, vans and “tip shrouds”; g. “Software” having all of the following: 1. Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and 2. Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions, which have been validated with actual aero gas turbine engine (experimental or production) performance data.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M19D1Code: 9D004Other “software” as follows: a. 2D or 3D viscous “software”, validated with wind tunnel or flight test data required for detailed engine flow modelling; b. “Software” for testing aero gas turbine engines, assemblies or components, specially designed to collect, reduce and analyse data in real time and capable of feedback control, including the dynamic adjustment of test articles or test conditions, as the test is in progress; c. “Software” specially designed to control directional solidification or single-crystal material growth in equipment specified in 9B001.a. or 9B001.c.; d. Not used; e. “Software” specially designed or modified for the operation of items specified in 9A012; f. “Software” specially designed to design the internal cooling passages of aero gas turbine blades, vans and “tip shrouds”; g. “Software” having all of the following: 1. Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and 2. Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions, which have been validated with actual aero gas turbine engine (experimental or production) performance data.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M19D1Code: 9D004“Software” specially designed or modified for the “production” of equipment specified in 9A001 to 9A119 or 9B.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2D2Code: 9D002“Software” specially designed or modified for the “production” of equipment specified in 9A001 to 9A119 or 9B.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M2D2Code: 9D002“Software” specially designed or modified for the “development” of equipment or “technology”, specified in 9A001 to 9A119, 9B or 9E003.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M3D3Code: 9D001“Software” specially designed or modified for the “development” of equipment or “technology”, specified in 9A001 to 9A119, 9B or 9E003.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M3D3Code: 9D001Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a “specific tensile strength” greater than 7,62 × 10 4 m and a “specific modulus” greater than 3,18 × 10 6 m. N.B.: SEE ALSO 1C010 AND 1C210. Note: The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (T g ), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M6C1Code: 9C110Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a “specific tensile strength” greater than 7,62 × 10 4 m and a “specific modulus” greater than 3,18 × 10 6 m. N.B.: SEE ALSO 1C010 AND 1C210. Note: The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (T g ), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent.
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M6C1Code: 9C110“Insulation” material in bulk form and “interior lining”, other than those specified in 9A008, for rocket motor cases usable in “missiles” or specially designed for ‘missiles’. Technical Note: In 9C108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3C2Code: 9C108“Insulation” material in bulk form and “interior lining”, other than those specified in 9A008, for rocket motor cases usable in “missiles” or specially designed for ‘missiles’. Technical Note: In 9C108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3C2Code: 9C108“Insulation” material in bulk form and “interior lining”, other than those specified in 9A008, for rocket motor cases usable in “missiles” or specially designed for ‘missiles’. Technical Note: In 9C108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3C1Code: 9C108“Insulation” material in bulk form and “interior lining”, other than those specified in 9A008, for rocket motor cases usable in “missiles” or specially designed for ‘missiles’. Technical Note: In 9C108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3C1Code: 9C108Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics: a. The capacity to handle more than 68 kN of thrust; or b. Capable of simultaneously measuring the three axial thrust components.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M15B3Code: 9B117Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics: a. The capacity to handle more than 68 kN of thrust; or b. Capable of simultaneously measuring the three axial thrust components.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M15B3Code: 9B117Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M19B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M19B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M1B1Code: 9B116Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or ‘missiles’. Technical Note: In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M1B1Code: 9B116Specially designed “production equipment” for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20B2Code: 9B115Specially designed “production equipment” for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M20B2Code: 9B115Specially designed “production equipment” for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3B2Code: 9B115Specially designed “production equipment” for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M3B2Code: 9B115Specially designed “production equipment” for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B2Code: 9B115Specially designed “production equipment” for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M2B2Code: 9B115Environmental chambers and anechoic chambers, as follows: a. Environmental chambers capable of simulating all the following flight conditions: 1. Having any of the following: a. Altitude equal to or greater than 15 km; or b. Temperature range from below 223 K (–50 ° C) to above 398 K (+125 °C); and 2. Incorporating, or ‘designed or modified’ to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured ‘bare table’, between 20 Hz and 2 kHz while imparting forces equal to or greater than 5 kN; Technical Notes: 1. 9B106.a.2. describes systems that are capable of generating a vibration environment with a single wave (e.g., a sine wave) and systems capable of generating a broad band random vibration (i.e., power spectrum). 2. In 9B106.a.2., ‘designed or modified’ means the environmental chamber provides appropriate interfaces (e.g., sealing devices) to incorporate a shaker unit or other vibration test equipment as specified in 2B116. 3. In 9B106.a.2. ‘bare table’ means a flat table, or surface, with no fixture or fittings. b. Environmental chambers capable of simulating the following flight conditions: 1. Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 μPa) or with a total rated acoustic power output of 4 kW or greater; and 2. Altitude equal to or greater than 15 km; or 3. Temperature range from below 223 K (–50 °C) to above 398 K (+125 °C).
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M15B4Code: 9B106Environmental chambers and anechoic chambers, as follows: a. Environmental chambers capable of simulating all the following flight conditions: 1. Having any of the following: a. Altitude equal to or greater than 15 km; or b. Temperature range from below 223 K (–50 ° C) to above 398 K (+125 °C); and 2. Incorporating, or ‘designed or modified’ to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured ‘bare table’, between 20 Hz and 2 kHz while imparting forces equal to or greater than 5 kN; Technical Notes: 1. 9B106.a.2. describes systems that are capable of generating a vibration environment with a single wave (e.g., a sine wave) and systems capable of generating a broad band random vibration (i.e., power spectrum). 2. In 9B106.a.2., ‘designed or modified’ means the environmental chamber provides appropriate interfaces (e.g., sealing devices) to incorporate a shaker unit or other vibration test equipment as specified in 2B116. 3. In 9B106.a.2. ‘bare table’ means a flat table, or surface, with no fixture or fittings. b. Environmental chambers capable of simulating the following flight conditions: 1. Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 μPa) or with a total rated acoustic power output of 4 kW or greater; and 2. Altitude equal to or greater than 15 km; or 3. Temperature range from below 223 K (–50 °C) to above 398 K (+125 °C).
Authority: EUProhibited Supply To: IRKPProgram: IREU Code: M15B4Code: 9B106‘Aerodynamic test facilities’ for speeds of Mach 0,9 or more, usable for ‘missiles’ and their subsystems. N.B.: SEE ALSO 9B005. Note: 9B105 does not control wind-tunnels for speeds of Mach 3 or less with dimension of the ‘test cross section size’ equal to or less than 250 mm. Technical Notes: 1. In 9B105 ‘aerodynamic test facilities’ includes wind tunnels and shock tunnels for the study of airflow over objects. 2. In Note to 9B105, ‘test cross section size’ means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest ‘test cross section’ location. ‘Test cross section’ is the section perpendicular to the flow direction. 3. In 9B105 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M15B2Code: 9B105‘Aerodynamic test facilities’ for speeds of Mach 0,9 or more, usable for ‘missiles’ and their subsystems. N.B.: SEE ALSO 9B005. Note: 9B105 does not control wind-tunnels for speeds of Mach 3 or less with dimension of the ‘test cross section size’ equal to or less than 250 mm. Technical Notes: 1. In 9B105 ‘aerodynamic test facilities’ includes wind tunnels and shock tunnels for the study of airflow over objects. 2. In Note to 9B105, ‘test cross section size’ means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest ‘test cross section’ location. ‘Test cross section’ is the section perpendicular to the flow direction. 3. In 9B105 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Authority: EUProhibited Supply To: IRProgram: IREU Code: M15B2Code: 9B105