Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or “spacecraft”, as follows: N.B.: SEE ALSO 1A002 AND 9A110. a. Components and structures, each exceeding 10 kg and specially designed for launch vehicles manufactured using any of the following: 1. “Composite” materials consisting of “fibrous or filamentary materials” specified in 1C0010.e. and resins specified in 1C008 or 1C009.b.; 2. Metal “matrix”“composites” reinforced by any of the following: a. Materials specified in 1C007; b. “Fibrous or filamentary materials” specified in 1C010; or c. Aluminides specified in 1C002.a.; or 3. Ceramic “matrix”“composite” materials specified in 1C007; Note: The weight cut-off is not relevant for nose cones.

Last Updated: April 11, 2026

9A010

M6A1

9A - Systems, Equipment and Components

EU Regulation No 267/2012

Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2.Technical Note:In Item 3.A.2., ‘combined cycle engines’ are the engines that employ two or more cycles of the following types of engines: gas-turbine engine (turbojet, turboprop, turbofan and turboshaft), ramjet, scramjet, pulse jet, pulse detonation engine, rocket motor (liquid/solid-propellant and hybrid).
Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.

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