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Key technology for airbreathing hypersonic aircraft.This paper reviews recent progress in the key hypersonic technologies, which has been good despite a relatively low priority. Successful hypersonic research engine tests have been made. Active cooling system analyses have shown potential for weight savings, alleviation of structural design problems, and long airframe life. Maturing computerized flow field theories permit optimizing engine-airframe performance. Adequate progress in the future requires an expanded technology program emphasizing hydrogen usage. A hydrogen fueled hypersonic research airplane is essential, providing critical flight data and operational experience.
Document ID
19730032829
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nagel, A. L.
Becker, J. V.
(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 73-58
Report Number: AIAA PAPER 73-58
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
73A17631
Distribution Limits
Public
Copyright
Other

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