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Refractory porcelain enamel passive-thermal-control coating for high-temperature superalloysStudy was conducted to match thermal expansion coefficients thereby preventing enamels from cracking. Report discusses various enamel coatings that are applied to two different high-temperature superalloys. Study may be of interest to manufacturers of chemical equipment, furnaces, and metal components intended for high-temperature applications.
Document ID
19730000215
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Levin, H. (Hughes Aircraft Co.)
Auker, B. H. (Hughes Aircraft Co.)
Gardos, M. N. (Hughes Aircraft Co.)
Date Acquired
August 7, 2013
Publication Date
August 1, 1973
Subject Category
Materials
Report/Patent Number
MFS-22324
Report Number: MFS-22324
Accession Number
73B10215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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