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Thermal control/oxidation resistant coatings for titanium-based alloysExtensive research and development efforts have been expended toward development of thermal control and environmental protection coatings for NASP and generic hypersonic vehicle applications. The objective of the coatings development activities summarized here was to develop light-weight coatings for protecting advanced titanium alloys from oxidation in hypersonic vehicle applications. A number of new coating concepts have been evaluated. Coated samples were exposed to static oxidation tests at temperatures up to 1000 C using a thermogravimetric apparatus. Samples were also exposed to simulated hypersonic flight conditions for up to 10 hr to determine their thermal and chemical stability and catalytic efficiency. The emittance of samples was determined before and after exposure to simulated hypersonic flight conditions.
Document ID
19930003269
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Clark, Ronald K.
(NASA Langley Research Center Hampton, VA, United States)
Wallace, Terryl A.
(NASA Langley Research Center Hampton, VA, United States)
Cunnington, George R.
(Lockheed Missiles and Space Co. Palo Alto, CA., United States)
Wiedemann, Karl E.
(Analytical Services and Materials, Inc. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Publication Information
Publication: Current Technology for Thermal Protection Systems
Subject Category
Composite Materials
Accession Number
93N12457
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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