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 5960-01-368-5874
NSN 5999-01-387-4924
NSN 5925-00-715-7831
NSN 5996-01-057-9023
NSN 6110-00-177-4657
NSN 5998-00-870-6723
NSN 5998-00-453-0072
NSN 6150-01-441-9359
NSN 5990-01-090-3232
NSN 6135-01-648-2284
NSN 6110-01-413-7764
NSN 6150-00-723-3839