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Economic study of multipurpose advanced high-speed transport configurationsA nondimensional economic examination of a parametrically-derived set of supersonic transport aircraft was conducted. The measure of economic value was surcharged relative to subsonic airplane tourist-class yield. Ten airplanes were defined according to size, payload, and speed. The price, range capability, fuel burned, and block time were determined for each configuration, then operating costs and surcharges were calculated. The parameter with the most noticeable influence on nominal surcharge was found to be real (constant dollars) fuel price increase. A change in SST design Mach number from 2.4 to Mach 2.7 showed a very small surcharge advantage (on the order of 1 percent for the faster aircraft). Configuration design compromises required for an airplane to operate overland at supersonic speeds without causing sonic boom annoyance result in severe performance penalties and require high (more than 100 percent) surcharges.
Document ID
19800005730
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
November 1, 1979
Subject Category
Economics And Cost Analysis
Report/Patent Number
NASA-CR-159126
D6-48725
Report Number: NASA-CR-159126
Report Number: D6-48725
Accession Number
80N13986
Funding Number(s)
CONTRACT_GRANT: NAS1-14623
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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