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 6135-00-100-8890
NSN 5996-00-954-0556
NSN 6240-01-128-2476
NSN 5915-00-232-3387
NSN 5975-00-723-0390
NSN 5996-01-055-5247
NSN 5935-01-562-2543
NSN 5855-00-058-1293
NSN 5855-01-147-6024
NSN 6645-01-129-8211
NSN 5965-00-999-4334
NSN 5930-01-091-8550