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 5945-00-759-0131
NSN 5905-01-426-4301
NSN 6685-01-149-2843
NSN 5895-00-553-8345
NSN 5915-01-514-5205
NSN 5960-01-599-9821
NSN 6685-01-275-6080
NSN 6220-01-616-9807
NSN 5996-01-053-6305
NSN 6135-01-139-1700
NSN 5945-00-248-6798
NSN 4140-01-534-8910