Accession Number : AD0164711

Title :   Integral Rocket/Ramjet Propulsion System with Axial Admission Ports.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Curran,Edward T.

Report Date : 07 JAN 1974

Pagination or Media Count : 17

Abstract : The patent application relates to the design of a ramjet engine whereby air injection ports and fuel injection systems are arranged in a manner to enhance flame stability.

Descriptors :   *Ramjet engines, *Combustors, Patents, Flames, Stability, Air intakes

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE