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- W1970788064 abstract "release. During the analysis of technology capabilities and requirements, it became apparent that capability would not be limited to advanced space Shuttle launch systems, but would also be applicable to supersonic-hy personic military aircraft and advanced hypersonic transport systems." @default.
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- W1970788064 date "1975-07-01" @default.
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- W1970788064 title "Propulsion Options for the Hypersonic Research Airplane" @default.
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- W1970788064 doi "https://doi.org/10.2514/3.59842" @default.
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