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 6150-00-548-3228
NSN 6135-01-442-7275
NSN 5895-00-153-2595
NSN 6150-00-595-6931
NSN 5945-00-105-8267
NSN 5930-01-365-5471
NSN 5925-01-617-5089
NSN 5930-00-406-1159
NSN 6650-01-103-7342
NSN 5998-01-230-6040
NSN 5985-00-713-4441
NSN 6105-01-524-1957