Accession Number : ADA952399

Title :   Application of a Liquid Propellant Rocket as a Turbojet Thrust Augmentation System.

Descriptive Note : Technical rept. on Phase 7,

Corporate Author : PRINCETON UNIV NJ DEPT OF AERONAUTICAL ENGINEERING

Personal Author(s) : Scott,John E. , Jr

Report Date : 29 APR 1953

Pagination or Media Count : 28

Descriptors :   *Ramjet engines, *Liquid propellant rocket engines, Thrust, Augmentation, Control systems, Rocket ramjets

Subject Categories : Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE