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Radiative, actively cooled panel tests resultsThe radiative, actively cooled panel designed to withstand a uniform incident heat flux of 136 kW/sq m to a 444 K surface temperature was evaluated. The test program consisted of preliminary static thermal mechanical loading and aerothermal flow tests. Test results are briefly discussed.
Document ID
19790013263
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shore, C. P.
(NASA Langley Research Center Hampton, VA, United States)
Nowak, R. J.
(NASA Langley Research Center Hampton, VA, United States)
Sharpe, E. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: Recent Advan. in Structures for Hypersonic Flight, Pt. 1
Subject Category
Structural Mechanics
Accession Number
79N21434
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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