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