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Composite engines for application to a single-stage-to-orbit vehicle (1975)

Brown, P. N. ; Piercy, T. G. ; Bendot, J. G.

In: CASI

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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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