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Date: 2020-12-14 Category: Not Applicable State: Union Government Country: Europe

Commission Delegated Regulation (EU) 2020/1749 of 7 October 2020 amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items

Issued by European Commission · Directorate-General for Trade and Economic Security

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Executive Summary & Key Takeaways

Executive Summary: The policy text pertains to telecommunications and information security. Specific parameters regarding missile payload capabilities, rocket systems, and components for cameras, including synchronizing electronics units and rotor assemblies, are outlined. Additionally, the text includes velocity interferometer systems, such as VISARs and DLIs. Key Points / Main Content: Telecommunications: Missile Payload and Range: Specifications apply to systems capable of delivering at least a 500 kg payload to a range of at least 300 km, with exceptions for certain rocket systems and non-weapon payloads. Space Launch Vehicles and Sounding Rockets: Parameters relate to vehicles specified in 9A004 and 9A104. Liquid Propellant Apogee Engines: Exceptions exist for satellite applications meeting specific nozzle and combustion chamber criteria. Information Security: Controlled Items: Covers items controlled at or below 5 kHz in real-time applications, with exceptions for guidance sets designed for missiles with a range under 300 km or manned aircraft. Rotating Mirrors: Mechanical rotating mirrors and their components, like synchronizing electronics units and rotor assemblies, are included. Velocity Interferometers: Systems such as VISARs and DLIs are also specified. Impact Analysis: Stakeholders: Manufacturers of telecommunications equipment and components, especially those involved with missile and rocket technology. Impact: Must adhere to the specifications and exceptions related to payload, range, and system design. Action Required: Review existing products and designs to ensure compliance with the specified parameters, especially regarding missile payload capabilities, rocket systems, and components for cameras and velocity interferometer systems. Stakeholders: Manufacturers of space launch vehicles and sounding rockets. Impact: Need to comply with the specifications related to space launch vehicles and sounding rockets. Action Required: Ensure components and systems adhere to guidelines, especially regarding liquid propellant apogee engines and those designed or modified for satellite applications. Stakeholders: Entities involved in information security and real-time applications. Impact: Impacted by the rules governing the control of items at or below 5 kHz in real-time applications. Action Required: Review existing products and practices to ensure compliance.

Key Entities Referenced

TELECOMMUNICATIONS: Refers to the sector related to communication technologies and services. This is Part 1 of the policy text. INFORMATION SECURITY: Refers to the protection of information assets from unauthorized access, use, disclosure, disruption, modification, or destruction. This is Part 2 of the policy text. missiles: Mentioned in the context of range and payload capabilities, specifically related to guidance sets and rocket systems. space launch vehicles: Mentioned in the context of payload delivery capabilities. Related to sounding rockets. sounding rockets: Mentioned in the context of payload delivery capabilities. Related to space launch vehicles. VISARs: Velocity interferometer systems for any reflector Doppler laser interferometers: Also known as DLIs. Mechanical rotating mirror: Component of high-speed cameras, including synchronizing electronics units and rotor assemblies.
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sets” designed for missiles with a range under 300 km or manned aircraftin 7A117 above ­ in 7A117 above. above above in 7A117, 7B003, 7B103 or 7D101 above in 7A117, 7B003 and 7B103 above above capable of delivering at least a 500 kg payload to a range of at least 300 km usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below delivering at least a 500 kg payload toexcept liquid propellant apogee engines designed or modified for satellite applications and having all of the following nozzle throat diameter of 20 mm or less; and 2. combustion chamber pressure of 15 bar or less. usable in “missiles”, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km usable in “missiles” as follows except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km except for reentry vehicles designed for non-weapon payloadsdelivering at least a 500 kg payload to above above above above above above above aboveμ μand above Mechanical rotating mirror Mechanical rotating mirror Note: In 6A203.a. components of such cameras include their synchronising electronics units and rotor assemblies consisting of turbines, mirrors and bearings. Note: 6A225 includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers).

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