Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. The engine designs were variations of the supercharged ejector ramjet engine. The resulting performance, weight, and drawings of each engine form a data base for establishing a potential of this class of composite engine to various missions, including the single-stage-to-orbit application. The impact of advanced technology in the design of the critical fan turbine was established. (Author)
Composite Engines for Application to a Single-Stage-to-Orbit Vehicle
1975
100 pages
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Englisch
A Rocket Powered Single-Stage-to-Orbit Launch Vehicle with U.S. and Soviet Engines
British Library Conference Proceedings | 1991
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