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