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Optimization of Rei-mullite Physical PropertiesMicromechanical and thermal modeling studies prove that ceramic fiber mullite materials is the only system capable of shuttle thermal protection to 1644 K. Hafnia pigmentated mullite surface coatings meet both orbital and reentry thermal radiative requirements for reuse without refurbishment. Thermal and mechanical models show growths potentials associated with the mullite system for a factor of 2 improvement in mechanical properties, and a factor of 2 to 3 reduction in thermal conductivity.
Document ID
19730024736
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tanzilli, R. A.
(General Electric Co. Philadelphia, PA, United States)
Musikant, S.
(General Electric Co. Philadelphia, PA, United States)
Bolinger, P. N.
(General Electric Co. Philadelphia, PA, United States)
Brazel, J. P.
(General Electric Co. Philadelphia, PA, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: NASA. Ames Res. Center Symp. on Reusable Surface Insulation for Space Shuttle, Vol. 1
Subject Category
Materials, Nonmetallic
Accession Number
73N33469
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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