Accession Number : ADD005005

Title :   Dual Manifold High Performance Throttleable Injector.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Addoms,John F ; McGough,Charles B

Report Date : 28 Mar 1978

Pagination or Media Count : 6

Abstract : This patent describes a dual manifold propellent injector having at least four distinct platelets in its configuration. The first two platelets constituting the primary and secondary fuel platelets; the third and fourth platelets constituting the primary and secondary oxidizer platelets. By proper valve throttling, the injector is capable of providing homogeneous, intimately mixed propellants at all thrust levels. (Author)

Descriptors :   *Patents, *Fuel injectors, *Liquid propellant rocket engines, Throttling, Manifolds(Engines), Plates

Subject Categories : Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE