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 5915-00-291-3736
NSN 5950-01-361-6194
NSN 6135-01-315-4328
NSN 6105-00-111-2546
NSN 6320-00-586-5641
NSN 6220-00-264-9473
NSN 6645-01-227-2036
NSN 6130-00-494-8451
NSN 2925-00-494-5537
NSN 5975-01-041-8298
NSN 5925-00-510-6922
NSN 5905-01-503-2562