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 5945-01-428-9317
NSN 5950-01-467-1765
NSN 5935-00-004-0232
NSN 5935-00-903-0627
NSN 5950-01-116-4155
NSN 6320-00-270-8222
NSN 6650-01-029-5414
NSN 5965-01-056-7225
NSN 6105-01-580-3338
NSN 5915-01-513-9122
NSN 6320-00-731-6134
NSN 5998-00-235-9676