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Advanced supersonic technology concept study: Hydrogen fueled configuration, summary reportConceptual designs of hydrogen fueled supersonic transport configurations for the 1990 time period were developed and compared with equivalent technology Jet A-1 fueled vehicles to determine the economic and performance potential of liquid hydrogen as an alternate fuel. Parametric evaluations of supersonic cruise vehicles with varying design and transport mission characteristics established the basis for selecting a preferred configuration. An assessment was made of the general viability of the selected concept including an evaluation of costs and environmental considerations, i.e., exhaust emissions and sonic boom characteristics. Technology development requirements and suggested implementation schedules are presented.
Document ID
19750013196
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brewer, G. D.
(Lockheed-California Co. Burbank, CA, United States)
Morris, R. E.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1975
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
LR-26322
NASA-CR-2534
Report Number: LR-26322
Report Number: NASA-CR-2534
Accession Number
75N21268
Funding Number(s)
CONTRACT_GRANT: NAS2-7732
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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