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Division [9B107] ‘Aerothermodynamic test facilities’, usable for ‘missiles’, ‘missile’ rocket propulsion systems, and reentry vehicles and equipment specified in 9A116, having any of the following characteristics:F1

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

  1. a..

    An electrical power supply equal to or greater than 5 MW; or

  2. b..

    A gas supply total pressure equal to or greater than 3 MPa.

Technical Notes:

1.

‘Aerothermodynamic test facilities’ include plasma arc jet facilities and plasma wind tunnels for the study of thermal and mechanical effects of airflow on objects.

2.

In 9B107 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

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.

Notes on Division [9B]

Textual amendments

F2

Annex 1 Section 9B Note inserted (20.5.2025) by The Export Control (Amendment) Regulations 2025 (S.I. 2025/532), regs. 1(2), 17(3)(a)