Accession Number : ADD001668

Title :   Liquid Fuel Injector System.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Dettling,Ronald F ; Nyberg,Donald G

Report Date : 29 Jul 1975

Pagination or Media Count : 5

Abstract : The patent relates to a method whereby a novel injector is provided for a variable thrust rocket engines using the annular-stream variable-area concept to give fast response and shut-off capability. This is accomplished by a simple arrangement of an annular metering sleeve which surrounds the central pintle such that a fuel and an oxidizer are separately and simultaneously metered to the combustion area. The metering sleeve, and contoured baffles forward of the opening, aid in providing a good mixture ratio control and performance.

Descriptors :   *Liquid propellant rocket engines, *Controllable thrust rocket engines, *Fuel injectors, *Patents, Fuel meters, Sleeves, Baffles, Pintles

Subject Categories : Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE