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 5990-01-074-6549
NSN 5905-01-288-0132
NSN 2925-01-116-6838
NSN 5855-00-832-9341
NSN 7035-00-392-5417
NSN 2925-01-303-5266
NSN 5990-00-184-5750
NSN 6685-01-446-3416
NSN 5985-00-019-0171
NSN 6130-00-328-0261
NSN 4140-01-346-3948
NSN 5935-01-195-8499