No other part numbers with same form, fit, and function found.
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 6145-00-170-7947
NSN 6320-01-329-2297
NSN 6220-00-302-8048
NSN 5895-01-578-6285
NSN 5935-00-818-7214
NSN 5835-01-278-4683
NSN 6620-01-461-3550
NSN 4140-01-133-0471
NSN 5905-01-446-8177
NSN 6685-00-012-3734
NSN 5999-00-290-5898
NSN 5855-01-287-6391