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 6610-01-589-5146
NSN 6130-01-149-5503
NSN 5985-00-740-7154
NSN 6240-01-582-5803
NSN 6650-01-066-9792
NSN 6110-01-292-3593
NSN 6320-01-308-0009
NSN 6220-00-262-0017
NSN 6130-01-032-4958
NSN 5945-00-362-0188
NSN 7035-01-589-2629
NSN 5905-01-318-3014