Accession Number : AD0164606

Title :   Ramjet with Integrated Rocket Boost Motor.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Leingang,John L.

Report Date : 13 SEP 1972

Pagination or Media Count : 5

Abstract : The patent application 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 :   *Booster rockets, *Ramjet engines, Patents, Rocket ramjets, Diffusers, Cruise missiles

Subject Categories : Air- and Space-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE