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 5950-00-604-8406
NSN 6145-01-644-0534
NSN 5915-00-997-3339
NSN 6150-01-566-2134
NSN 5855-01-580-8155
NSN 5996-01-305-4892
NSN 4140-01-126-7368
NSN 5996-01-118-5320
NSN 6150-01-595-4102
NSN 6110-01-425-5355
NSN 5975-01-361-8080
NSN 7035-01-033-3007