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  • 1975-1979  (1)
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    Publication Date: 2019-07-13
    Description: 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.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: NASA-CR-2613 , S-1325
    Format: application/pdf
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