NASA NTRS · 19880000108
Thermal Response Of Composite Insulation
Abstract
Engineering 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.
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Stewart, David A., Leiser, Daniel B., Smith, Marnell, Kolodziej, Paul. 1988-02-01. Thermal Response Of Composite Insulation. https://ntrs.nasa.gov/citations/19880000108
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