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 5905-00-617-4798
NSN 5965-00-281-0319
NSN 5999-01-422-4506
NSN 5990-00-644-3365
NSN 6150-01-042-4942
NSN 5935-00-155-3020
NSN 5999-00-824-7579
NSN 5945-00-304-9501
NSN 6130-00-412-8191
NSN 4140-01-436-1878
NSN 5835-01-481-4204
NSN 5935-01-660-8324