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Design and fabrication of a radiative actively cooled honeycomb sandwich panelThe mass of a radiative actively cooled panel was compared to the mass of a bare actively cooled panel designed to the same conditions and constraints. The approach was to design and optimize a 0.61 x 6.1 m full scale panel which combines radiative and active cooling to control structural temperatures to levels compatible with use of lightweight materials and to fabricate a 0.61 x 1.22 m panel for performance testing. Results of the design and optimization of the full scale radiative actively cooled structural panel, including radiative concept selection, final configuration details, test panel description, and conclusions are summarized.
Document ID
19790013262
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Koch, L. C.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA. Langley Res. Center Recent Advan. in Structures for Hypersonic Flight, Pt. 1
Subject Category
Structural Mechanics
Accession Number
79N21433
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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