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“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 2.A., 2.B. or 2.D.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 2.A., 2.B. or 2.D.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of systems in 2.A.1.f.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of systems in 2.A.1.f.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of systems in 2.A.1.e.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of systems in 2.A.1.e.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of subsystems or equipment specified in 2.A.1.b.3.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of subsystems or equipment specified in 2.A.1.b.3.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software”, specially designed or modified for the “use” of ‘guidance sets’ specified in 2.A.1.d. ´ ´
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software”, specially designed or modified for the “use” of ‘guidance sets’ specified in 2.A.1.d. ´ ´
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of rocket motors or engines specified in 2.A.1.c.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of rocket motors or engines specified in 2.A.1.c.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of “production facilities” specified in 2.B.1.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of “production facilities” specified in 2.B.1.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production equipment” specially designed for the subsystems specified in 2.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production equipment” specially designed for the subsystems specified in 2.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production facilities” specially designed for the subsystems specified in 2.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production facilities” specially designed for the subsystems specified in 2.A.
Authority: GBProhibited Supply To: IRProgram: UK-INUComplete subsystems usable in the systems specified in 1.A., as follows: a. Individual rocket stages usable in the systems specified in 1.A.; b. Re-entry vehicles, and equipment designed or modified therefor, usable in the systems specified in 1.A., as follows, except as provided in the Note below 2.A.1. for those designed for non-weapon payloads: 1. Heat shields, and components therefor, fabricated of ceramic or ablative materials; 2. Heat sinks and components therefor , fabricated of light-weight, high heat capacity materials; 3. Electronic equipment specially designed for re-entry vehicles; c. Solid propellant rocket motors, hybrid rocket motors or liquid propellant rocket engines, usable in the systems specified in 1.A., having a total impulse capacity equal to or greater than 1.1 x 10 6 Ns; d. ‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving system accuracy of 3.33% or less of the “range” (e.g. a ‘CEP’ of 10 km or less at a “range” of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a “range” under 300 km or manned aircraft; e. Thrust vector control sub-systems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the “range”/”payload” capability of systems specified in 1.A.; f. Weapon or warhead safing, arming, fuzing, and firing mechanisms, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for systems other than those specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INUComplete subsystems usable in the systems specified in 1.A., as follows: a. Individual rocket stages usable in the systems specified in 1.A.; b. Re-entry vehicles, and equipment designed or modified therefor, usable in the systems specified in 1.A., as follows, except as provided in the Note below 2.A.1. for those designed for non-weapon payloads: 1. Heat shields, and components therefor, fabricated of ceramic or ablative materials; 2. Heat sinks and components therefor , fabricated of light-weight, high heat capacity materials; 3. Electronic equipment specially designed for re-entry vehicles; c. Solid propellant rocket motors, hybrid rocket motors or liquid propellant rocket engines, usable in the systems specified in 1.A., having a total impulse capacity equal to or greater than 1.1 x 10 6 Ns; d. ‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving system accuracy of 3.33% or less of the “range” (e.g. a ‘CEP’ of 10 km or less at a “range” of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a “range” under 300 km or manned aircraft; e. Thrust vector control sub-systems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the “range”/”payload” capability of systems specified in 1.A.; f. Weapon or warhead safing, arming, fuzing, and firing mechanisms, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for systems other than those specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 1.A., 1.B., or 1.D.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 1.A., 1.B., or 1.D.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” which coordinates the function of more than one subsystem, specially designed or modified for “use” in systems specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” which coordinates the function of more than one subsystem, specially designed or modified for “use” in systems specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of “production facilities” specified in 1.B.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of “production facilities” specified in 1.B.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production facilities” specially designed for the systems specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Production facilities” specially designed for the systems specified in 1.A.
Authority: GBProhibited Supply To: IRProgram: UK-INUComplete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones) capable of delivering at least a 500 kg “payload” to a “range” of at least 300 km.
Authority: GBProhibited Supply To: IRProgram: UK-INUComplete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones) capable of delivering at least a 500 kg “payload” to a “range” of at least 300 km.
Authority: GBProhibited Supply To: IRProgram: UK-INUComplete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets) capable of delivering at least a 500 kg “payload” to a “range” of at least 300 km.
Authority: GBProhibited Supply To: IRProgram: UK-INUComplete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets) capable of delivering at least a 500 kg “payload” to a “range” of at least 300 km.
Authority: GBProhibited Supply To: IRProgram: UK-INU"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 6.A. through 6.D.
Authority: GBProhibited Supply To: IRProgram: UK-INU"Technology" according to the Technology Controls for the "development", "production" or "use" of equipment, material or "software" specified in 6.A. through 6.D.
Authority: GBProhibited Supply To: IRProgram: UK-INUHigh explosive substances or mixtures, containing more than 2 % by weight of any of the following: a. Cyclotetramethylenetetranitramine (HMX ) (CAS 2691-41-0); b. Cyclotrimethylenetrinitramine (RDX) (CAS 121-82-4); c. Triaminotrinitrobenzene (TATB) (CAS 3058-38-6); d. Hexanitrostilbene (HNS) (CAS 20062-22-0); or e. Any explosive with a crystal density greater than 1.8 g/cm 3 and having a detonation velocity greater than 8000 m/s.
Authority: GBProhibited Supply To: IRProgram: UK-INUHigh explosive substances or mixtures, containing more than 2 % by weight of any of the following: a. Cyclotetramethylenetetranitramine (HMX ) (CAS 2691-41-0); b. Cyclotrimethylenetrinitramine (RDX) (CAS 121-82-4); c. Triaminotrinitrobenzene (TATB) (CAS 3058-38-6); d. Hexanitrostilbene (HNS) (CAS 20062-22-0); or e. Any explosive with a crystal density greater than 1.8 g/cm 3 and having a detonation velocity greater than 8000 m/s.
Authority: GBProhibited Supply To: IRProgram: UK-INUNeutron generator systems, including tubes, having both of the following characteristics: a. Designed for operation without an external vacuum system; and b. Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction.
Authority: GBProhibited Supply To: IRProgram: UK-INUNeutron generator systems, including tubes, having both of the following characteristics: a. Designed for operation without an external vacuum system; and b. Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction.
Authority: GBProhibited Supply To: IRProgram: UK-INUPulse discharge capacitors having either of the following sets of characteristics: a. 1. Voltage rating greater than 1.4 kV; 2. Energy storage greater than 10 J; 3. Capacitance greater than 0.5 μF; and 4. Series inductance less than 50 nH; or b. 1. Voltage rating greater than 750 V; 2. Capacitance greater than 0.25 μF; and 3. Series inductance less than 10 nH.
Authority: GBProhibited Supply To: IRProgram: UK-INUPulse discharge capacitors having either of the following sets of characteristics: a. 1. Voltage rating greater than 1.4 kV; 2. Energy storage greater than 10 J; 3. Capacitance greater than 0.5 μF; and 4. Series inductance less than 50 nH; or b. 1. Voltage rating greater than 750 V; 2. Capacitance greater than 0.25 μF; and 3. Series inductance less than 10 nH.
Authority: GBProhibited Supply To: IRProgram: UK-INU