Description:

Lgm-30, guided missile specific usage design, 1337-v480 dod ammunition code, ex1988100992 dot registration code, 0.9972 storage pounds net explosive weight.

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.