Description:

Agm-69a end item identification, ex1988100987 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.