Publikationsdatum:
2019-07-13
Beschreibung:
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.
Schlagwort(e):
SPACECRAFT PROPULSION AND POWER
Materialart:
NASA-CR-2613
,
S-1325
Format:
application/pdf
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