Consists of 1 ea exit cone, insulated 117568802; 1 ea nozzle subassembly 1175086-21
An item designed with a constricting throat section and a divergent section. The constricting throat section compresses the propellant gases and maintains the pressure within the thrust chamber of the rocket motor by limiting the flow of gases. The divergent section controls the expansion of the gases causing increased thrust.
Classification: Parts for guided missiles
NSN 7035-01-366-5912
NSN 5895-01-307-7379
NSN 5895-01-576-2098
NSN 5910-01-511-0065
NSN 5935-00-737-4925
NSN 5925-00-482-0854
NSN 6685-00-369-0279
NSN 6135-00-422-3967
NSN 6320-01-056-1164
NSN 5925-00-939-4979
NSN 5996-01-168-2746
NSN 5945-00-795-4824