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 6135-01-142-2417
NSN 5895-01-533-4439
NSN 5960-00-357-3043
NSN 5905-01-257-9575
NSN 5925-00-235-8524
NSN 5920-01-649-4887
NSN 6130-01-227-9683
NSN 7035-01-287-7781
NSN 5998-00-479-9817
NSN 6650-00-879-5834
NSN 6685-01-600-0433
NSN 6645-01-302-5408