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Toward a second-generation supersonic transport.A number of promising avenues of research and development are considered in relation to an advanced supersonic transport which has improved range/payload characteristics and lower airport noise and sonic boom than current-generation supersonic transports. The prospects for advanced technology suggest that a high lift-to-drag-ratio configuration incorporating advanced materials and control concepts and utilizing a variable-cycle engine or perhaps an advanced dry turbojet, will yield an advanced supersonic transport which is economically viable and socially acceptable. Hydrogen fuel offers great promise for future supersonic aircraft, however, the formidable problems associated with the use of such fuel probably precludes its use on any near term second-generation supersonic transport. The state of technology in some of the areas discussed is not very far advanced and, consequently, a major effort will be required to bring these technologies to a state of readiness on a timely basis.
Document ID
19730032806
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Loftin, L. K., Jr.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 73-15
Report Number: AIAA PAPER 73-15
Meeting Information
Meeting: Annual Meeting and Technical Display
Location: Washington, DC
Start Date: January 8, 1973
End Date: January 10, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A17608
Distribution Limits
Public
Copyright
Other

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