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 5960-01-271-7239
NSN 4140-00-218-3579
NSN 6610-01-189-3001
NSN 6650-01-348-5448
NSN 5895-01-561-8657
NSN 7035-01-150-6303
NSN 5965-01-196-7760
NSN 7035-01-150-6303
NSN 4140-01-522-7230
NSN 4140-00-232-9859
NSN 6650-00-995-5741
NSN 5950-00-969-6876