Model: 1338-VN40
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 1338-VN40 NSN 1338-01-174-5707
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsFreight 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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