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 5930-01-371-2248
NSN 5975-00-099-9312
NSN 5998-01-100-2428
NSN 6220-01-634-0660
NSN 6145-00-841-1382
NSN 5975-01-255-8914
NSN 5999-01-485-5770
NSN 5945-01-254-2633
NSN 5930-01-191-6399
NSN 5950-01-316-5349
NSN 7035-01-061-4754
NSN 5985-00-407-5968