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A NASA Lewis comparative propulsion system assessment for the High-Speed Civil TransportThe topics covered include the following: High Speed Research (HSR) Propulsion System Studies; HRS System Study flowpath; design point aircraft sizing - no noise constraint; impact of noise constraint; noise impact on aircraft size; takeoff gross weight assessment; impact of High Speed Civil Transport (HSCT) high-altitude flyover noise; HSR NO(x) reduction status; current assessment of HSCT ozone depletion; influence of non-optimum cruise altitude on range; and influence of subsonic leg on range.
Document ID
19940028971
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Berton, Jeffrey J. (NASA Lewis Research Center Cleveland, OH, United States)
Haller, William J. (NASA Lewis Research Center Cleveland, OH, United States)
Seidel, Jonathan A. (NASA Lewis Research Center Cleveland, OH, United States)
Senick, Paul F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Publication Information
Publication: NASA. Langley Research Center, First Annual High-Speed Research Workshop, Part 2
Subject Category
Aircraft Propulsion And Power
Accession Number
94N33477
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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