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Thermal Response Of Composite InsulationEngineering model gives useful predictions. Pair of reports presents theoretical and experimental analyses of thermal responses of multiple-component, lightweight, porous, ceramic insulators. Particular materials examined destined for use in Space Shuttle thermal protection system, test methods and heat-transfer theory useful to chemical, metallurgical, and ceramic engineers needing to calculate transient thermal responses of refractory composites.
Document ID
19880000108
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Stewart, David A.
(NASA Ames Research Center, Moffett Field, Calif.)
Leiser, Daniel B.
(NASA Ames Research Center, Moffett Field, Calif.)
Smith, Marnell
(NASA Ames Research Center, Moffett Field, Calif.)
Kolodziej, Paul
(Informatics, Inc.)
Date Acquired
August 13, 2013
Publication Date
February 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 2
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
ARC-11680
Accession Number
88B10108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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