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Engine/airframe compatibility studies for supersonic cruise aircraftTechnology assessment studies were conducted to provide an updated technology base from which an advanced supersonic cruise aircraft can be produced with a high probability of success. An assessment of the gains available through the application of advanced technologies in aerodynamics, propulsion, acoustics, structures, materials, and active controls is developed. The potential market and range requirements as well as economic factors including payload, speed, airline operating costs, and airline profitability are analyzed. The conceptual design of the baseline aircraft to be used in assessing the technology requirements is described.
Document ID
19750010149
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
MDC-J4478
NASA-CR-132610
Report Number: MDC-J4478
Report Number: NASA-CR-132610
Accession Number
75N18221
Funding Number(s)
CONTRACT_GRANT: NAS1-13229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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