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Multiwall TPSA study of multiwall TPS as an alternative to LRSI for the space shuttle indicated that vented multiwall, with foil thicknesses limited to those used in multiwall fabricated to date, is some what heavier than LRSI. With reduced foil thicknesses, multiwall TPS may equal the weight of LRSI. Metallic conduction through multiwall TPS transfered less heat than gas conduction or radiation. Radiation heat transfer was greatest at high temperatures; however, the number of layers selected can significantly reduce radiation. At low-to-intermediate temperatures, gas conduction transfered the most heat through multiwall TPS. Gas conduction may be eliminated by evacuation of panels. Oxidation rates required a trade of foil thickness against life.
Document ID
19790013269
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jackson, L. R.
(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. 2
Subject Category
Structural Mechanics
Accession Number
79N21440
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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