Accession Number : ADD000689
Title : Reverse Flow Aft Inlet Ramjet System.
Descriptive Note : Patent Application,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Curran,Edward T
Report Date : 11 Mar 1975
Pagination or Media Count : 29
Abstract : The patent application relates generally to integral rocket/ramjets and, in particular, to ramjets having multiple, aft-mounted air inlets and used to propel missiles.
Descriptors : *Guided missiles, *Ramjet engines, Ramjet inlets, Rocket engines, Air intakes, Air launched, Patents
Subject Categories : Guided Missiles
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE