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“Production equipment”, other than that described in 4.B.3., and specially designed components therefor, for the production, handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 4.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production equipment”, other than that described in 4.B.3., and specially designed components therefor, for the production, handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 4.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production equipment”, and specially designed components therefor, for the “production”, handling or acceptance testing of liquid propellants or propellant constituents specified in 4.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production equipment”, and specially designed components therefor, for the “production”, handling or acceptance testing of liquid propellants or propellant constituents specified in 4.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment, materials or “software” specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8. , 3.A.9., 3.B., 3.C. or 3.D.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment, materials or “software” specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8. , 3.A.9., 3.B., 3.C. or 3.D.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “development” of equipment specified in 3.A.2., 3.A.3. or 3.A.4.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “development” of equipment specified in 3.A.2., 3.A.3. or 3.A.4.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of equipment specified in 3.A.1., 3.A.2., 3.A.4., 3.A.5., 3.A.6. or 3.A.9.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of equipment specified in 3.A.1., 3.A.2., 3.A.4., 3.A.5., 3.A.6. or 3.A.9.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of “production facilities” and flow forming machines specified in 3.B.1. or 3.B.3.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of “production facilities” and flow forming machines specified in 3.B.1. or 3.B.3.
Authority: GBProhibited Supply To: IRProgram: UK-INU‘Insulation’ material in bulk form usable for rocket motor cases in the systems specified in 1.A. or specially designed for systems specified in 19.A.1. or 19.A.2.
Authority: GBProhibited Supply To: IRProgram: UK-INU‘Insulation’ material in bulk form usable for rocket motor cases in the systems specified in 1.A. or specially designed for systems specified in 19.A.1. or 19.A.2.
Authority: GBProhibited Supply To: IRProgram: UK-INU‘Interior lining’ usable for rocket motor cases in the systems specified in 1.A. or specially designed for systems specified in 19.A.1. or 19.A.2.
Authority: GBProhibited Supply To: IRProgram: UK-INU‘Interior lining’ usable for rocket motor cases in the systems specified in 1.A. or specially designed for systems specified in 19.A.1. or 19.A.2.
Authority: GBProhibited Supply To: IRProgram: UK-INUFlow-forming machines, and specially designed components therefor, which: a. According to the manufacturers technical specification can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; and b. Have more than two axes which can be co-ordinated simultaneously for contouring control.
Authority: GBProhibited Supply To: IRProgram: UK-INUFlow-forming machines, and specially designed components therefor, which: a. According to the manufacturers technical specification can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; and b. Have more than two axes which can be co-ordinated simultaneously for contouring control.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production equipment” specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9 . or 3.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production equipment” specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9 . or 3.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production facilities” specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9. or 3.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production facilities” specially designed for equipment or materials specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9. or 3.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU‘Turboprop engine systems’ specially designed for the systems in 1.A.2. or 19.A.2., and specially designed components therefor, having a maximum power greater than 10 kW (achieved uninstalled at sea level standard conditions), excluding civil certified engines. ‘ ’
Authority: GBProhibited Supply To: IRProgram: UK-INU‘Turboprop engine systems’ specially designed for the systems in 1.A.2. or 19.A.2., and specially designed components therefor, having a maximum power greater than 10 kW (achieved uninstalled at sea level standard conditions), excluding civil certified engines. ‘ ’
Authority: GBProhibited Supply To: IRProgram: UK-INULiquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INULiquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INURadial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics: a. An inner ring bore diameter between 12 and 50 mm; b. An outer ring outside diameter between 25 and 100 mm; and c. A width between 10 and 20 mm.
Authority: GBProhibited Supply To: IRProgram: UK-INURadial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics: a. An inner ring bore diameter between 12 and 50 mm; b. An outer ring outside diameter between 25 and 100 mm; and c. A width between 10 and 20 mm.
Authority: GBProhibited Supply To: IRProgram: UK-INUSpecially designed components for hybrid rocket motors specified in 2.A.1.c. and 20.A.1.b.
Authority: GBProhibited Supply To: IRProgram: UK-INUSpecially designed components for hybrid rocket motors specified in 2.A.1.c. and 20.A.1.b.
Authority: GBProhibited Supply To: IRProgram: UK-INULiquid and slurry propellant (including oxidisers) control systems, and specially designed components therefor, usable in the systems specified in 1.A., designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.
Authority: GBProhibited Supply To: IRProgram: UK-INULiquid and slurry propellant (including oxidisers) control systems, and specially designed components therefor, usable in the systems specified in 1.A., designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.
Authority: GBProhibited Supply To: IRProgram: UK-INUStaging mechanisms, separation mechanisms, and interstages therefor, usable in the systems specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INUStaging mechanisms, separation mechanisms, and interstages therefor, usable in the systems specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INURocket motor cases, ‘insulation’ components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INURocket motor cases, ‘insulation’ components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INURamjet/scramjet/pulse jet/ ’ combined cycle engines ’ , including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2.
Authority: GBProhibited Supply To: IRProgram: UK-INURamjet/scramjet/pulse jet/ ’ combined cycle engines ’ , including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2.
Authority: GBProhibited Supply To: IRProgram: UK-INUTurbojet and turbofan engines, as follows: a. Engines having both of the following characteristics: 1. ‘ Maximum thrust value ’ greater than 400 N (achieved un-installed) excluding civil certified engines with a ‘ maximum thrust value ’ greater than 8.89 kN (achieved un-installed); and 2. Specific fuel consumption of 0.15 kg N -1 h -1 or less (at maximum continuous power at sea level static and standard conditions); Technical Note: In 3.A.1.a.1., ‘maximum thrust value’ is the manufacturer’s demonstrated maximum thrust for the engine type un-installed. The civil type certified thrust value will be equal to or less than the manufacturer’s demonstrated maximum thrust for the engine type. b. Engines designed or modified for systems specified in 1.A. or 19.A.2., regardless of thrust or specific fuel consumption.
Authority: GBProhibited Supply To: IRProgram: UK-INUTurbojet and turbofan engines, as follows: a. Engines having both of the following characteristics: 1. ‘ Maximum thrust value ’ greater than 400 N (achieved un-installed) excluding civil certified engines with a ‘ maximum thrust value ’ greater than 8.89 kN (achieved un-installed); and 2. Specific fuel consumption of 0.15 kg N -1 h -1 or less (at maximum continuous power at sea level static and standard conditions); Technical Note: In 3.A.1.a.1., ‘maximum thrust value’ is the manufacturer’s demonstrated maximum thrust for the engine type un-installed. The civil type certified thrust value will be equal to or less than the manufacturer’s demonstrated maximum thrust for the engine type. b. Engines designed or modified for systems specified in 1.A. or 19.A.2., regardless of thrust or specific fuel consumption.
Authority: GBProhibited Supply To: IRProgram: UK-INU