NASA NTRS · 19800006816
Hypersonic cruise aircraft propulsion integration study, volume 2
Abstract
Conceptual vehicle configuration and propulsion approach for a Mach 6 transport aircraft capable of carring 200 passengers 9260 km was investigated. Wind tunnel test data for various hypersonic transport configurations were examined. Canidates for baseline reference vehicles were selected. An explanation of technical methods which were used and configuration details which were significant in the final vehicle concept are given.
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Morris, R. E., Brewer, G. D.. 1979-09-01. Hypersonic cruise aircraft propulsion integration study, volume 2. https://ntrs.nasa.gov/citations/19800006816
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