Accession Number : ADD004915

Title :   Thrust Management Control Propulsion System.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON D C

Personal Author(s) : LeFebvre,Clarence A ; Cabezut,Joseph M , Jr

Report Date : 13 Sep 1977

Pagination or Media Count : 3

Abstract : A control system for supplying uncured propellant into the combustion chamber of a missile. The system includes a moving injector cooperating with a pressurized putty-like uncured propellant. This combination provides the missile with a propulsion system having rapid wide range throttling, shut off and restart capabilities. (Author)

Descriptors :   *Patents, *Solid propellants, Gas generating systems, Injectors, Combustion

Subject Categories : Solid Propellant Rocket Engines
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE