O/a width 3.84 in
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.
Classification: Parts for guided missiles
NSN 6105-00-399-1352
NSN 6220-01-351-1555
NSN 5945-01-141-5570
NSN 5975-01-042-3439
NSN 6145-01-221-3105
NSN 5920-01-009-1307
NSN 5835-00-543-1325
NSN 5835-01-384-3206
NSN 6130-00-919-5653
NSN 5975-01-300-0761
NSN 6240-01-600-7489
NSN 6620-00-767-8151