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 6650-01-063-8356
NSN 2925-00-054-3550
NSN 5965-01-479-8214
NSN 5996-00-938-4878
NSN 6145-01-210-9472
NSN 5905-01-145-3031
NSN 5915-01-481-3025
NSN 5905-00-345-0688
NSN 2925-01-391-9247
NSN 5975-01-424-9263
NSN 6320-01-006-6138
NSN 5965-01-549-4942