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 6650-01-376-1692
NSN 5998-00-932-5589
NSN 5960-01-447-7074
NSN 6650-01-365-1894
NSN 7035-01-649-8977
NSN 6620-00-005-5624
NSN 6240-00-519-3399
NSN 6320-01-607-1491
NSN 5925-01-215-1386
NSN 4140-01-322-3227
NSN 5990-00-627-5151
NSN 6685-01-142-9276