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Reusable surface insulation thermal protection systems test evaluation statusChanges in coating morphology of mullite, silica, and ceramic mullite fiber at two heating rates are described followed by a discussion of the changes in surface chemistry that occur during convective heating tests. Subsequently, the surface chemistry changes observed are compared to similar data obtained from radiantly heated coatings and the significance of the difference between the results is discussed. Finally, the changes in chemistry of the coatings in cross section before and after convectively heated cyclic testing are discussed and the significance of surface chemistry changes are described. Results indicate that the thermal conductivity of mullite surface insulation is higher than that of silica insulation, based on thermal response data. Acoustic excitation of cracked silica tiles does not lead to catastrophic failure such as spallation or tile loss. Cracks in mullite material after thermal exposure lead to fracturing of the coating and surface insulation material after acoustic excitation.
Document ID
19730024756
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Strouhal, G.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Tillian, D. J.
(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. 2
Subject Category
Materials, Nonmetallic
Accession Number
73N33489
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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