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Composite Engines for Application to a Single-stage-to-orbit Vehicle

Joseph G. BendotPhilip N. BrownThomas G. Piercy

出版	National Aeronautics and Space Administration, 1975
URL	http://books.google.com.hk/books?id=UM1jMzGLtMMC&hl=&source=gbs_api

註釋

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.