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Radiative, ablative, and active cooling thermal protection studies for the leading edge of a fixed-straight wing space shuttlePerformance prediction of fixed wing leading edges radiative, ablative and active cooling thermal protection systems and system weights comparison for space shuttle entry mission
Document ID
19710045533
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Curry, D. M.
Gomez, A. V.
Johnston, C. G.
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 71-445
Report Number: AIAA PAPER 71-445
Meeting Information
Meeting: THERMOPHYSICS CONFERENCE
Location: TULLAHOMA, TN
Start Date: April 26, 1971
End Date: April 28, 1971
Sponsors: AIAA
Accession Number
71A26230
Distribution Limits
Public
Copyright
Other

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