NSN 1420-00-911-1960 009111960

1420-00-911-1960 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.20513370087Guided Missile and Space Vehicle Explosive Propulsion Units, Solid Fuel; and Components13380083Guided Missile and Space Vehicle Inert Propulsion Units, Solid Fuel; and Components13400048Rockets, Rocket Ammunition and Rocket Components13770056Cartridge and Propellant Actuated Devices and Components

Part Alternates: 009111960

Ammunition and Explosives | Guided Missile and Space Vehicle Inert Propulsion Units, Solid Fuel; and Components