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Processing of Rigidized Rei-mullite Insulative CompositesSystematic development and evaluation of ceramic fiber Mullite are summarized: (1) Major reductions in thermal protection system weight have been achieved by reducing the density and thermal conductivity of the insulation by 20 and 25 percent; (2) already adequate structural margins-of-safety have been greatly enhanced by increasing the tensile strength and strain-to-failure capabilities of the insulation by factors of 3 and 2; (3) cost effectiveness has been increased through the achievement of a high degree of uniformity and reproducibility of properties and through process simplification and binder modifications; and (4) maximization of multimission capability at surface temperatures of 1644 K has been achieved through firing cycle adjustments and the development of a material with high dimensional stability.
Document ID
19730024730
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gebhardt, J. J.
(General Electric Co. Philadelphia, PA, United States)
Gorsuch, P. D.
(General Electric Co. Philadelphia, PA, United States)
Braun, M. A.
(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
73N33463
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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