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 5990-01-541-5632
NSN 6145-00-170-7947
NSN 5855-01-609-5749
NSN 6685-00-700-9751
NSN 4140-01-056-4453
NSN 5985-01-067-3752
NSN 6650-01-069-8211
NSN 5999-01-539-4110
NSN 5920-01-280-9147
NSN 5915-01-136-6265
NSN 5960-01-240-3266
NSN 5920-00-578-3750