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Division [9A006] Systems and components, specially designed for liquid rocket propulsion systems, as follows:F1

Changes not yet applied. Later legislation changes this provision in ways not yet written into the text below:

NB:

SEE ALSO 9A106, 9A108 AND 9A120.

  1. a..

    Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems, F2designed to restrict cryogenic fluid losses to less than 30 % per year;

  2. b..

    F3Cryogenic containers or closed-cycle refrigeration systems, designed to maintain or produce temperatures less than or equal to 100 K (- 173.15° C);

  3. c..

    Slush hydrogen storage or transfer systems;

  4. d..

    High pressure (exceeding 17,5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems;

  5. e..

    High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor;

  6. f..

    Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders);

  7. g..

    Liquid propellant injectors with individual orifices of 0,381 mm or smaller in diameter (an area of 1,14 × 10–3 cm2 or smaller for non-circular orifices) and specially designed for liquid rocket engines;

  8. h..

    One-piece carbon-carbon thrust chambers or one-piece carbon-carbon exit cones, with densities exceeding 1,4 g/cm3 and tensile strengths exceeding 48 MPa.

Annotations

Textual amendments

F1

Substituted by 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.

F2

Words in Annex 1 Entry 9A006 substituted (1.4.2024) by The Export Control (Amendment) Regulations 2024 (S.I. 2024/346), regs. 1(1), 3(20)(a)

F3

Words in Annex 1 Entry 9A006 substituted (1.4.2024) by The Export Control (Amendment) Regulations 2024 (S.I. 2024/346), regs. 1(1), 3(20)(b)