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Results of RSI Thermal-structural AnalysisThermostructural comparisons of mullite and silica reusable surface insulation materials for space shuttle application show that mullite is much more subject to thermal stress failure than silica composite materials.
Document ID
19730024765
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pigg, O. E. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: Symp. on Reusable Surface Insulation for Space Shuttle, Vol. 3
Subject Category
Thermodynamics And Combustion
Accession Number
73N33498
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19730024757Collected WorksSymposium on Reusable Surface Insulation for Space Shuttle. Volume 3: Thermal Protection System Design and Optimization
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