Accession Number : ADD006482

Title :   Solid Protrusion Jet Vector Control System.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON DC

Personal Author(s) : Dunaway ,J C ; Clayton,Bobby J

Report Date : 29 May 1979

Pagination or Media Count : 7

Abstract : This report describes a thrust vector control system for rockets that use a solid protrusion inserted into the exit cone of the rocket nozzle. This protrusion is inserted linearly into one side of the rocket exit nozzle and creates a side force for use in control of the missile in flight.

Descriptors :   *Patent applications, *Thrust vector control systems, *Control rods, Rocket nozzles, Exits, Walls, Protuberances, Retractable, Fluidic control, Modulators, Pulse duration modulation

Subject Categories : Fluidics and Fluerics
      Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE