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 6130-01-265-1021
NSN 6220-01-604-8283
NSN 5960-01-474-4843
NSN 5990-01-024-9659
NSN 6650-00-890-0480
NSN 5915-01-371-2906
NSN 5855-00-004-0904
NSN 6685-00-319-3497
NSN 6150-01-356-2424
NSN 6240-01-256-8132
NSN 6610-01-589-5146
NSN 6145-00-943-0729