Accession Number : ADD000349
Title : AFT Inlet Ramjet Powered Missile.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Wilkinson,David B
Report Date : 29 Oct 1974
Pagination or Media Count : 3
Abstract : The patent relates to a solid fuel ramjet powered missile having the air inlets positioned adjacent the aft end of the fuel grain with a channel provided adjacent the fuel grain to provide primary air into the forward end of the fuel grain. The secondary air is supplied directly to the secondary combustor. A valve is provided in the primary air flow channel to control the air flow into the fuel grain.
Descriptors : *Guided missiles, *Ramjet engines, *Patents, Solid fuels, Combustors, Air flow, Throttling
Subject Categories : Guided Missiles
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE