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 6105-00-615-9979
NSN 6620-01-438-0415
NSN 5905-01-351-5678
NSN 6110-01-529-6338
NSN 5996-01-054-3226
NSN 6110-01-478-8466
NSN 6110-01-506-0595
NSN 7035-01-191-2822
NSN 6145-00-423-1563
NSN 6105-01-134-2025
NSN 5975-01-350-3425
NSN 5945-01-413-0967