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