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 6650-01-101-6622
NSN 5945-00-290-1779
NSN 5950-01-134-5425
NSN 6320-01-497-3116
NSN 5930-00-646-0707
NSN 5925-01-660-7206
NSN 6685-01-095-5554
NSN 5920-01-508-8500
NSN 6150-00-536-0274
NSN 6105-01-020-3558
NSN 6685-00-198-0384
NSN 5905-01-110-0847