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9A010

Aerospace and Propulsion

Category 9Group AWassenaar Arrangement2 thresholds

Description

b. Components and structures, specially designed for launch vehicle propulsion systems specified in 9.A.5. to 9.A.9. manufactured using any of the following: 1. "Fibrous or filamentary materials" specified in 1.C.10.e. and resins specified in 1.C.8. or 1.C.9.b.; 2. Metal "matrix" "composite" materials reinforced by any of the following:

Control Thresholds

Reference	Parameter	Threshold
9A010.d	Pulsed liquid rocket engines with thrust-to-weight ratios	>= 1 kN/kg
9A010.d	tios equal to or more than 1 kN/kg and a ‘response time’ of	< 30 ms

Sub-entries (16)

9A010.a

Materials specified in 1.C.7.;

9A010.b

"Fibrous or filamentary materials" specified in 1.C.10.; or

9A010.c

Aluminides specified in 1.C.2.a.; or 3. Ceramic "matrix" "composite" materials specified in 1.C.7.;

9A010.a.1

"Composite" materials consisting of "fibrous or filamentary materials" specified in 1C010.e. and resins specified in 1C008 or 1C009.b.;

9A010.a.2

Metal "matrix""composites" reinforced by any of the following:

9A010.a.2.a

Materials specified in 1C007;

9A010.a.2.b

"Fibrous or filamentary materials" specified in 1C010; or

9A010.a.2.c

Aluminides specified in 1C002.a.; or

9A010.a.3

Ceramic "matrix""composite" materials specified in 1C007;

9A010.b.1

"Fibrous or filamentary materials" specified in 1C010.e. and resins specified in 1C008 or 1C009.b.;

9A010.b.2

Metal "matrix""composites" reinforced by any of the following:

9A010.b.2.a

Materials specified in 1C007;

9A010.b.2.b

"Fibrous or filamentary materials" specified in 1C010; or

9A010.b.2.c

Aluminides specified in 1C002.a.; or

9A010.b.3

Ceramic "matrix""composite" materials specified in 1C007;

9A010.d

Pulsed liquid rocket engines with thrust-to-weight ratios equal to or more than 1 kN/kg and a ‘response time’ of less than 30 ms.

Pulsed liquid rocket engines with thrust-to-weight ratios: >= 1 kN/kgtios equal to or more than 1 kN/kg and a ‘response time’ of: < 30 ms

Product Examples

Carbon-carbon composite combustion chamber for Ariane launcher engine
Ceramic matrix composite nozzle for SpaceX Raptor rocket engine
Aluminum fiber-reinforced tank structure for Vega launcher
Composite booster segments for Rocket Lab Electron rocket

Related CN customs codes (indicative)

88039000 84129080 73089059 68151010

Applicable Notes

General Technology Note (GTN)

The export of 'technology' which is 'required' for the 'development', 'production' or 'use' of items controlled in Categories 0 to 9 is controlled according to the provisions in each Category. 'Techno...

General Software Note (GSN)

The Lists do not control 'software' which is either: 1. Generally available to the public by being: a. Sold from stock at retail selling points, without restriction, by means of: (1) Over-the-counter ...

Category 9 - Aerospace and Propulsion

This category covers aerospace vehicles, engines, and related equipment. It includes gas turbine engines (controlled based on thrust-to-weight ratio, specific fuel consumption, inlet temperature), roc...

Catch-All Clause - Article 4 of Regulation (EU) 2021/821

Article 4(1): An authorisation shall be required for the export of dual-use items not listed in Annex I if the exporter has been informed by the competent authority that the items in question are or m...

Cyber-Surveillance Catch-All - Article 5 of Regulation (EU) 2021/821

Article 5(1): An authorisation shall be required for the export of cyber-surveillance items not listed in Annex I if the exporter has been informed by the competent authority that the items in questio...

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9A010

See also