O/a diameter 1.5 in; designed to yaw the ejection seat away from the aircraft centerline; initiated by a squib which is electrically initiated by the recovery sequencer after the ejection seat has left the seat carriage
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 6220-00-375-0473
NSN 6145-00-293-5097
NSN 5999-00-433-4258
NSN 5999-01-157-1644
NSN 5925-01-442-8589
NSN 7035-01-641-4634
NSN 5985-01-620-0263
NSN 5990-00-170-4239
NSN 6650-00-754-2276
NSN 6135-01-503-1688
NSN 6650-01-289-0524
NSN 5950-01-289-3340