Other parts suitable for use solely or principally with the apparatus of headings 8524 to 8528

Optical Sensors as follows: a. Image intensifier tubes and specially designed components therefor, as follows: 1. Image intensifier tubes having all the following: a. A peak response in wavelength range exceeding 400 nm, but not exceeding 1 050 nm; b. A microchannel plate for electron image amplification with a hole pitch (centre-to-centre spacing) of less than 25 μm; and c. Having any of the following: 1. An S-20, S-25 or multialkali photocathode; or 2. A GaAs or GaInAs photocathode; 2. Specially designed microchannel plates having both of the following characteristics: a. 15 000 or more hollow tubes per plate; and b. Hole pitch (centre-to-centre spacing) of less than 25 μm b. Direct view imaging equipment operating in the visible or infrared spectrum, incorporating image intensifier tubes having the characteristics of the image intensifier tube included in this control.

‘Satellite navigation system’ equipment, including aerials and antennas suitable for the reception of GNSS signals, and parts thereof

Radar systems, equipment and major components, other than those specified in the CML or in Regulation (EU) 2021/821, and specially designed components therefor, as follows: a. Airborne radar equipment, other than those specified in the CML or in Regulation (EU) 2021/821, and specially designed components therefor; b. ‘Space-qualified’‘laser’ radar or Light Detection and Ranging (LIDAR) equipment specially designed for surveying or for meteorological observation; c. Millimeter wave enhanced vision radar imaging systems specially designed for rotary wing aircraft and having all of the following: 1. Operates at a frequency of 94 GHz; 2. An average output power of less than 20 mW; 3. Radar beam width of 1 degree; and 4. Operating range equal to or greater than 1 500 m

Radio navigational aid apparatus for ‘aircraft’ and specially designed components thereof

‘Flight termination’ systems and specifically designed components . Note: this control covers digital and analogic communications standards for Flight Termination Systems, including encrypted operational modes. Technical notes: 1. For the purposes of this control, ‘flight termination’ can involve a controlled descent, self-destruction, or detonation of the warhead to minimize the risk of collateral damage 2. For the purposes of this control, components include ground and on board equipment, command exciters, encoders, amplifier controllers, command verification receivers, amplifiers, transmitters, decoders and receivers.

Electrical machinery and equipment and parts thereof; sound recorders and reproducers, television image and sound recorders and reproducers, and parts and accessories of such articles

Other parts suitable for use solely or principally with the apparatus of headings 8524 to 8528High Priority

Program information