Model: 1337-V199
Rocket Motor85.260 inches overall length, lgm30, guided missile specific usage design, 1337-v199 dod ammunition code, ex1988100972 dot registration code.
Properties:
A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber and exhaust nozzle, and that carries its own solid oxidizer-fuel combination from which hot gases are generated by combustion and expanded through a nozzle. See also rocket motor cluster.
Part 1337-V199 NSN 1337-00-236-4866
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPricing & Availability Check
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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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