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Thermal and mechanical properties of advanced, high temperature ceramic-composite insulationIt is found that the mechanical properties of fibrous refractory composite insulation (FRCI) can be improved if a higher calcination temperature is used before final processing. The results also reveal that a higher density FRCI containing 60 wt pct aluminoborosilicate fibers will exhibit minimal surface recession at 1480 C in a convective-heating environment. Another finding is that the material performance in the convective-heating environment is limited by the coating and the temperature capability of its emittance agent. A table is included giving the coating compositions used with the composite insulation and tested in the convectively heated environment at a surface temperature of 1480 C.
Document ID
19840030721
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Leiser, D. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Smith, M.
(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 12, 2013
Publication Date
August 1, 1983
Publication Information
Publication: Ceramic Engineering and Science Proceedings
Volume: 4
ISSN: 0196-6219
Subject Category
Composite Materials
Accession Number
84A13508
Distribution Limits
Public
Copyright
Other

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