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 6645-01-063-0399
NSN 6610-00-705-9502
NSN 5990-00-172-7951
NSN 6685-01-437-9697
NSN 5910-00-597-5824
NSN 5855-00-079-2370
NSN 5975-00-518-2129
NSN 5855-00-482-9876
NSN 5895-01-213-7323
NSN 5910-01-429-8931
NSN 5998-00-418-4206
NSN 5945-00-005-6941