Accession Number : ADD009345

Title :   Gaseous Secondary Injection Thrust Vector Control Device.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON DC

Personal Author(s) : Dunaway,J C ; Jacobs,Paul L

Report Date : 25 Mar 1982

Pagination or Media Count : 12

Abstract : Apparatus for modulating the thrust vector of a rocket motor by injecting hot gas into the divergent section of the rocket nozzle and modulating injection of the hot gas by varying the flow from a solid propellant gas generator by controlling its flow rate with a vortex throttling valve arrangement. (Author)

Descriptors :   *Patent applications, *Thrust vector control systems, *Rocket engines, Inventions, Rocket nozzles, Secondary injection, Hot gases, Gas generating systems, Vortices, Throttling, Valves, Modulation, Solid propellants

Subject Categories : Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE