Description:

Lgm-30, guided missile specific usage design, 1337-v196 dod ammunition code, ex1988100935 dot registration code, 1.3 department of defense hazard class division hazardous material classification 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.