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Low sonic boom design and performance of a Mach 2.4/1.8 overland high speed civil transportThis paper describes the design features of a Douglas Mach 2.4/1.8 Low Sonic Boom High Speed Civil Transport (HSCT) configuration developed for NASA. The configuration is designed to fly over water at Mach 2.4 for highest productivity and economic worth, and fly over land at Mach 1.8 with reduced sonic boom loudness.
Document ID
19920076745
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morgenstern, John M. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1992
Publication Information
Publication: NASA. Langley Research Center, High-Speed Research: Sonic Boom, Volume 2
Subject Category
Aircraft Design, Testing And Performance
Accession Number
92X10699
Funding Number(s)
CONTRACT_GRANT: NAS1-19345
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19920076740Collected WorksHigh-Speed Research: Sonic Boom, volume 2
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