No other part numbers with same form, fit, and function found.
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 6240-01-414-9529
NSN 6150-01-252-3996
NSN 6110-01-395-6364
NSN 5855-01-307-1159
NSN 6130-01-417-2165
NSN 6110-01-454-9390
NSN 6130-01-518-0271
NSN 5965-01-331-6378
NSN 4140-01-446-3525
NSN 6145-01-347-2403
NSN 5990-00-840-6571
NSN 6620-01-531-3250