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 5855-00-908-6402
NSN 6645-00-262-7448
NSN 5950-01-438-6415
NSN 7035-01-063-8753
NSN 5920-01-286-4297
NSN 6135-01-592-4139
NSN 5950-00-144-4139
NSN 5930-01-253-1520
NSN 6135-00-945-0015
NSN 6650-00-023-1638
NSN 5975-00-469-1443
NSN 6650-01-612-1832