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 5855-01-053-9684
NSN 5975-00-225-1881
NSN 5998-01-078-2500
NSN 6240-01-352-3642
NSN 5935-01-571-7247
NSN 5925-00-019-9047
NSN 6105-00-840-6433
NSN 6645-00-189-7075
NSN 5855-01-020-7982
NSN 5985-00-618-4745
NSN 6145-01-092-8201
NSN 5999-00-785-8555