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Last Updated: April 11, 2026

Hybrid rocket propulsion systems having any of the following: N.B.: SEE ALSO 9A109 AND 9A119. a. Total impulse capacity exceeding 1,1 MNs; or b. Thrust levels exceeding 220 kN in vacuum exit conditions.

Code

9A009

EU Code

M2A1c1

Category

ANNEX III - CATEGORY 9 — AEROSPACE AND PROPULSION

Subcategory

9A - Systems, Equipment and Components

Prohibited Supply To
IR
Authority
EU
Document

EU Regulation No 267/2012

Notes
  • Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 10 6 Ns;
  • Rocket propulsion subsystems, not specified in 2.A.1., usable in the systems specified in 19.A.1., as follows:1. Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 8,41 × 105Ns, but less than 1,1 × 106Ns;2. Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 8,41 × 105Ns, but less than 1,1 × 106Ns;
Program information
Program information

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