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Chemical and morphological changes of reusable surface insulation coatings as a function of convectively heated cyclic testingThe effects of convective heating upon reusable surface insulation coatings were studied utilizing scanning electron microscopy, X-ray fluorescence, and X-ray diffraction. Samples of coated silica, mullite, and ceramic mullite fiber were cycled in an arc plasma stream up to 15 times for 15 minutes per cycle at surface temperatures simulating those on the space shuttle vehicle. The surfaces of ceramic mullite fiber and mullite coatings were roughened substantially by the convectively heated environment while the silica was significantly smoothed after testing. Scanning electron microscopy also showed surface cracking of varying degrees in all of the coatings. The surface chemistry of the coatings as examined by X-ray fluorescence revealed that significant changes in composition were occurring during cycling, particularly within the mullite coating.
Document ID
19730024755
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leiser, D. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Stewart, D. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Goldstein, H. E.
(NASA Ames Research Center Moffett Field, CA, 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
73N33488
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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