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 6130-01-455-2838
NSN 5960-01-018-8596
NSN 5920-01-473-5245
NSN 6240-01-061-7359
NSN 6240-01-597-1021
NSN 5835-01-576-9013
NSN 5935-01-198-4694
NSN 5835-00-007-6824
NSN 5895-01-488-6242
NSN 5935-01-083-5876
NSN 6105-00-379-9011
NSN 5999-00-222-4431