Search Sanctioned Goods & HS Codes

10K+ items found

On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use in wind tunnels designed for speeds of Mach 1,2 or more.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.015
Code: 9B005
On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use in wind tunnels designed for speeds of Mach 1,2 or more.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.015
Code: 9B005
Tools, dies or fixtures, for the solid-state joining of ‘superalloy’, titanium or intermetallic airfoil-to-disk combinations described in paragraph 2 of the section below entitled ‘Technology’ for gas turbines.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.014
Code: 9B004
Tools, dies or fixtures, for the solid-state joining of ‘superalloy’, titanium or intermetallic airfoil-to-disk combinations described in paragraph 2 of the section below entitled ‘Technology’ for gas turbines.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.014
Code: 9B004
Equipment specially designed for the ‘production’ or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.013
Code: 9B003
Equipment specially designed for the ‘production’ or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.013
Code: 9B003
On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment specially designed for the ‘development’ of gas turbine engines, assemblies or components and incorporating any of the ‘technologies’ specified in paragraph 2 (b) or 2 (c) of the section below entitled ‘Technology’.
Authority: EU
Prohibited Supply To: KP
Program: KP
EU Code: IX.A9.012
Code: 9B002
On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment specially designed for the ‘development’ of gas turbine engines, assemblies or components and incorporating any of the ‘technologies’ specified in paragraph 2 (b) or 2 (c) of the section below entitled ‘Technology’.
Authority: EU
Prohibited Supply To: KP
Program: KP
EU Code: IX.A9.012
Code: 9B002
‘Unmanned Aerial Vehicles’ (‘UAVs’), unmanned ‘airships’, related equipment and components, as follows: (a) ‘UAVs’ or unmanned ‘airships’, designed to have controlled flight out of the direct ‘natural vision’ of the ‘operator’ and having any of the following: 1. Having all of the following: a. A maximum ‘endurance’ greater than or equal to 30 minutes but less than 1 hour; and b. Designed to take off and have stable controlled flight in wind gusts equal to or exceeding 46,3 km/h (25 knots); or 2. A maximum ‘endurance’ of 1 hour or greater; Technical notes: 1. For the purposes of the item above, ‘operator’ is a person who initiates or commands the ‘UAV’ or unmanned ‘airship’ flight. 2. For the purposes of the item above, ‘endurance’ is to be calculated for International Standard Atmosphere (ISA) conditions (ISO 2533:1975) at sea level in zero wind. 3. For the purposes of the item above, ‘natural vision’ means unaided human sight, with or without corrective lenses. (b) Related equipment and components, as follows: 1. Equipment or components, specially designed to convert a manned ‘aircraft’ or a manned ‘airship’ to a ‘UAV’ or unmanned ‘airship’, specified in item (a) above; 2. Air breathing reciprocating or rotary internal combustion type engines, specially designed or modified to propel ‘UAVs’ or unmanned ‘airships’, at altitudes above 15 240 metres (50 000 feet).
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.011
Code: 9A012
‘Unmanned Aerial Vehicles’ (‘UAVs’), unmanned ‘airships’, related equipment and components, as follows: (a) ‘UAVs’ or unmanned ‘airships’, designed to have controlled flight out of the direct ‘natural vision’ of the ‘operator’ and having any of the following: 1. Having all of the following: a. A maximum ‘endurance’ greater than or equal to 30 minutes but less than 1 hour; and b. Designed to take off and have stable controlled flight in wind gusts equal to or exceeding 46,3 km/h (25 knots); or 2. A maximum ‘endurance’ of 1 hour or greater; Technical notes: 1. For the purposes of the item above, ‘operator’ is a person who initiates or commands the ‘UAV’ or unmanned ‘airship’ flight. 2. For the purposes of the item above, ‘endurance’ is to be calculated for International Standard Atmosphere (ISA) conditions (ISO 2533:1975) at sea level in zero wind. 3. For the purposes of the item above, ‘natural vision’ means unaided human sight, with or without corrective lenses. (b) Related equipment and components, as follows: 1. Equipment or components, specially designed to convert a manned ‘aircraft’ or a manned ‘airship’ to a ‘UAV’ or unmanned ‘airship’, specified in item (a) above; 2. Air breathing reciprocating or rotary internal combustion type engines, specially designed or modified to propel ‘UAVs’ or unmanned ‘airships’, at altitudes above 15 240 metres (50 000 feet).
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.011
Code: 9A012
Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or ‘spacecraft’, as follows: (a) Components and structures, specially designed for launch vehicle propulsion systems manufactured using any of the following: 1. ‘Fibrous or filamentary materials’; 2. Metal ‘matrix’‘composite’ materials; or 3. Ceramic ‘matrix’‘composite’ materials.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.010
Code: 9A010
Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or ‘spacecraft’, as follows: (a) Components and structures, specially designed for launch vehicle propulsion systems manufactured using any of the following: 1. ‘Fibrous or filamentary materials’; 2. Metal ‘matrix’‘composite’ materials; or 3. Ceramic ‘matrix’‘composite’ materials.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.010
Code: 9A010
Hybrid rocket propulsion systems.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.009
Code: 9A009
Hybrid rocket propulsion systems.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.009
Code: 9A009
Components specially designed for solid rocket propulsion systems, as follows: (a) Insulation and propellant bonding systems, using liners to provide a ‘strong mechanical bond’ or a barrier to chemical migration between the solid propellant and case insulation material; (b) Filament-wound ‘composite’ motor cases exceeding 0,61 m in diameter or having ‘structural efficiency ratios (PV/W)’ exceeding 25 km; Technical note: ‘Structural efficiency ratio (PV/W)’ is the burst pressure (P) multiplied by the vessel volume (V) divided by the total pressure vessel weight (W). (c) Nozzles with thrust levels exceeding 45 kN or nozzle throat erosion rates of less than 0,075 mm/s; (d) Movable nozzle or secondary fluid injection thrust vector control systems, capable of any of the following: 1. Omni-axial movement exceeding ± 5°; 2. Angular vector rotations of 20°/s or more; or 3. Angular vector accelerations of 40°/s 2 or more.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.008
Code: 9A008
Components specially designed for solid rocket propulsion systems, as follows: (a) Insulation and propellant bonding systems, using liners to provide a ‘strong mechanical bond’ or a barrier to chemical migration between the solid propellant and case insulation material; (b) Filament-wound ‘composite’ motor cases exceeding 0,61 m in diameter or having ‘structural efficiency ratios (PV/W)’ exceeding 25 km; Technical note: ‘Structural efficiency ratio (PV/W)’ is the burst pressure (P) multiplied by the vessel volume (V) divided by the total pressure vessel weight (W). (c) Nozzles with thrust levels exceeding 45 kN or nozzle throat erosion rates of less than 0,075 mm/s; (d) Movable nozzle or secondary fluid injection thrust vector control systems, capable of any of the following: 1. Omni-axial movement exceeding ± 5°; 2. Angular vector rotations of 20°/s or more; or 3. Angular vector accelerations of 40°/s 2 or more.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.008
Code: 9A008
Solid rocket propulsion systems.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.007
Code: 9A007
Solid rocket propulsion systems.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.007
Code: 9A007
Systems and components, specially designed for liquid rocket propulsion systems, as follows: (a) Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems, specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30 % per year; (b) Cryogenic containers or closed-cycle refrigeration systems capable of providing temperatures of 100 K (– 173 °C) or less for ‘aircraft’ capable of sustained flight at speeds exceeding Mach 3, launch vehicles or ‘spacecraft’; (c) Slush hydrogen storage or transfer systems; (d) High-pressure (exceeding 17,5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems; (e) High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor; (f) Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders); (g) Liquid propellant injectors with individual orifices of 0,381 mm or smaller in diameter (an area of 1,14 × 10 – 3 cm 2 or smaller for non-circular orifices) and specially designed for liquid rocket engines; (h) One-piece carbon-carbon thrust chambers or one-piece carbon-carbon exit cones, with densities exceeding 1,4 g/cm 3 and tensile strengths exceeding 48 MPa
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.006
Code: 9A006
Systems and components, specially designed for liquid rocket propulsion systems, as follows: (a) Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems, specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30 % per year; (b) Cryogenic containers or closed-cycle refrigeration systems capable of providing temperatures of 100 K (– 173 °C) or less for ‘aircraft’ capable of sustained flight at speeds exceeding Mach 3, launch vehicles or ‘spacecraft’; (c) Slush hydrogen storage or transfer systems; (d) High-pressure (exceeding 17,5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems; (e) High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor; (f) Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders); (g) Liquid propellant injectors with individual orifices of 0,381 mm or smaller in diameter (an area of 1,14 × 10 – 3 cm 2 or smaller for non-circular orifices) and specially designed for liquid rocket engines; (h) One-piece carbon-carbon thrust chambers or one-piece carbon-carbon exit cones, with densities exceeding 1,4 g/cm 3 and tensile strengths exceeding 48 MPa
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.006
Code: 9A006
Liquid rocket propulsion systems.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.005
Code: 9A005
Liquid rocket propulsion systems.
Authority: EU
Prohibited Supply To: IRKP
Program: KP
EU Code: IX.A9.005
Code: 9A005
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
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
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
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
‘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
‘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
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
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
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
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
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
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
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
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
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
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
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
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

Search sanctioned goods across UK and EU export control lists in one place. This tool covers dual-use items, military equipment, and other restricted goods and technologies. Each entry includes the specific goods description, issuing authority, countries subject to import or export restrictions, and the relevant sanctions programme. This helps compliance and trade teams determine whether an item is subject to import or export prohibitions.

Use the filters to narrow results by authority, target state, or sanctions programme. Whether you’re checking a single HS code or reviewing an entire category, the sanctioned goods list is updated as new designations and programme consolidated changes are published.

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On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use in wind tunnels designed for speeds of Mach 1,2 or more.

On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use in wind tunnels designed for speeds of Mach 1,2 or more.

Tools, dies or fixtures, for the solid-state joining of ‘superalloy’, titanium or intermetallic airfoil-to-disk combinations described in paragraph 2 of the section below entitled ‘Technology’ for gas turbines.

Tools, dies or fixtures, for the solid-state joining of ‘superalloy’, titanium or intermetallic airfoil-to-disk combinations described in paragraph 2 of the section below entitled ‘Technology’ for gas turbines.

Equipment specially designed for the ‘production’ or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.

Equipment specially designed for the ‘production’ or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.

Hybrid rocket propulsion systems.

Hybrid rocket propulsion systems.

Solid rocket propulsion systems.

Solid rocket propulsion systems.

Liquid rocket propulsion systems.

Liquid rocket propulsion systems.

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).

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).

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

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

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.

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.

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On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use in wind tunnels designed for speeds of Mach 1,2 or more.

On-line (real-time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use in wind tunnels designed for speeds of Mach 1,2 or more.

Tools, dies or fixtures, for the solid-state joining of ‘superalloy’, titanium or intermetallic airfoil-to-disk combinations described in paragraph 2 of the section below entitled ‘Technology’ for gas turbines.

Tools, dies or fixtures, for the solid-state joining of ‘superalloy’, titanium or intermetallic airfoil-to-disk combinations described in paragraph 2 of the section below entitled ‘Technology’ for gas turbines.

Equipment specially designed for the ‘production’ or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.

Equipment specially designed for the ‘production’ or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.

Hybrid rocket propulsion systems.

Hybrid rocket propulsion systems.

Solid rocket propulsion systems.

Solid rocket propulsion systems.

Liquid rocket propulsion systems.

Liquid rocket propulsion systems.

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).

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).

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

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

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.

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.