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 6135-01-503-1688
NSN 6685-01-614-0487
NSN 5990-00-186-2445
NSN 5965-01-444-3098
NSN 5920-01-068-0178
NSN 6240-00-616-4029
NSN 6220-01-320-7585
NSN 5985-00-241-9282
NSN 6620-00-555-3992
NSN 5915-01-026-8569
NSN 6610-01-470-0165
NSN 5985-01-258-5943