Description:

8.000 inches overall length, 1.690 inch size designation, av-8a aircraft specific usage design, 1377-m743 dod ammunition code, ex1988050634 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.