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 5998-00-577-3519
NSN 5855-00-327-2112
NSN 6150-00-035-4573
NSN 2925-01-523-3607
NSN 6105-01-245-2376
NSN 5905-00-965-8710
NSN 5925-00-171-0307
NSN 5930-01-125-5843
NSN 6645-00-051-4591
NSN 7035-01-590-6755
NSN 7035-01-146-1578
NSN 6110-01-411-7392