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Hydrogen plasma tests of some insulating coating systems for the nuclear rocket thrust chamberSeveral plasma-sprayed and slurry-coated insulating coating systems were evaluated for structural stability in a low-pressure hot hydrogen environment at a maximum heat flux of 19.6 million watts/sq meter. The heat was provided by an electric-arc plasma generator. The coating systems consisted of a number of thin layers of metal oxides and/or metals. The materials included molybdenum, nichrome, tungsten, alumina, zirconia, and chromia. The study indicates potential usefulness in this environment for some coatings, and points up the need for improved coating application techniques.
Document ID
19720007145
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Current, A. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Grisaffe, S. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Wycoff, K. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2461
E-6565
Accession Number
72N14795
Funding Number(s)
PROJECT: RTOP 112-29
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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