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.
NSN 6220-01-525-3241
NSN 6320-00-500-4172
NSN 6645-01-577-2306
NSN 5975-00-642-8959
NSN 5999-01-153-7199
NSN 5910-01-155-8664
NSN 5998-01-460-7873
NSN 6130-00-052-2143
NSN 6685-00-335-2964
NSN 6135-01-327-2092
NSN 7035-01-083-0282
NSN 5945-00-577-9606