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 6685-01-441-3145
NSN 6610-01-282-9953
NSN 5895-00-004-4993
NSN 5835-01-235-1125
NSN 5935-01-094-3744
NSN 5996-01-175-0902
NSN 5975-00-108-6464
NSN 6610-01-044-4740
NSN 5915-00-993-9833
NSN 6150-01-415-0916
NSN 5910-01-368-6785
NSN 5895-00-538-6231