Evaluation of three thermal protection systems in a hypersonic high-heating-rate environment induced by an elevon deflected 30/̊ /

Evaluation of three thermal protection systems in a hypersonic high-heating-rate environment induced by an elevon deflected 30/̊ /

Bibliographic Details
Main Author: Taylor, Allan H.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Other Authors: Weinstein, Irving
Format: Government Document Book
Language:English
Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1977.
Series:NASA technical memorandum ; 74077
Subjects:
Hypersonic planes.
Thermodynamics.

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