Model: 1131AS105
Rocket Motor Exhaust NozzleProperties:
An item designed with a constricting throat section and a divergent section. The constricting throat section compresses the propellant gases and maintains the pressure within the thrust chamber of the rocket motor by limiting the flow of gases. The divergent section controls the expansion of the gases causing increased thrust.
Part 1131AS105 NSN 1338-01-094-2810
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
Freight Classification
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Schedule B and Export
- Schedule B: 9306900060
- SITC: 89129
- End Use: Tanks, artillery, missiles, rockets, guns and ammunition
- NAICS: 336415
- USDA: 1
Freight Class: Parts for guided missiles
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