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Division [9A007] Solid rocket propulsion systems having any of the following:F1

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

NB:

SEE ALSO 9A107 AND 9A119.

  1. a..

    Total impulse capacity exceeding 1,1 MNs;

  2. b..

    Specific impulse of 2,4 kNs/kg or more, when the nozzle flow is expanded to ambient sea level conditions for an adjusted chamber pressure of 7 MPa;

  3. c..

    Stage mass fractions exceeding 88 % and propellant solid loadings exceeding 86 %;

  4. d..

    Components specified in 9A008; or

  5. e..

    Insulation and propellant bonding systems, using direct-bonded motor designs to provide a F2“strong mechanical bond” or a barrier to chemical migration between the solid propellant and case insulation material.

    F3...

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 9A007.e substituted (20.5.2025) by The Export Control (Amendment) Regulations 2025 (S.I. 2025/532), regs. 1(2), 17(2)(c)(i)

F3

Annex 1 Entry 9A.007.e Technical Note omitted (20.5.2025) by virtue of The Export Control (Amendment) Regulations 2025 (S.I. 2025/532), regs. 1(2), 17(2)(c)(ii)