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Mode Transition in Integral Ramjet Rocket Propulsion Systems.

Beecroft,William G., Petersen,Russell E.

Abstract

An analytical study of mode transition in the integral ramjet-rocket class of propulsion system was conducted. A baseline design was selected and used for analysis. The several factors affecting the engine aerothermodynamic performance during mode transition were evaluated. A quantitative evaluation method was established to aid in design of future engines of this class. Specific developmental recommendations are made. (Author)

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Available abstract

Key concepts: Ramjet, Propulsion, Aerospace engineering, Rocket (weapon), Mode (computer interface), Liquid-propellant rocket, Aeronautics, Engineering