Accession Number : ADD001920

Title :   Ramjet with Integrated Rocket Boost Motor.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Leingang,John L

Report Date : 26 Aug 1975

Pagination or Media Count : 5

Abstract : The patent relates to a combination rocket motor ramjet engine having the rocket motor located in the ramjet inlet diffuser. All or part of the rocket portion of the apparatus remaining after rocket booster burnout are ejected by air pressure in the diffuser inlet to permit the diffuser to supply ram air for the ramjet engine.

Descriptors :   *Rocket ramjets, *Patents, Ramjet engines, Booster rocket engines, Diffusers, Ramjet inlets, Ejection

Subject Categories : Jet and Gas Turbine Engines
      Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE