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Effectiveness of Diffusion Barrier Coatings for Mo-Re Embedded in C/SiC and C/CAdvanced high-temperature cooling applications may often require the elevated-temperature capability of carbon/silicon carbide or carbon/carbon composites in combination with the hermetic capability of metallic tubes. In this paper, the effects of C/SiC and C/C on tubes fabricated from several different refractory metals were evaluated. Though Mo, Nb, and Re were evaluated in the present study, the primary effort was directed toward two alloys of Mo-Re, namely, arc cast Mo-41Re and powder metallurgy Mo-47.5Re. Samples of these refractory metals were subjected to either the PyC/SiC deposition or embedding in C/C. MoSi2(Ge), R512E, and TiB2 coatings were included on several of the samples as potential diffusion barriers. The effects of the processing and thermal exposure on the samples were evaluated by conducting burst tests, microhardness surveys, and scanning electron microscopic examination (using either secondary electron or back scattered electron imaging and energy dispersive spectroscopy). The results showed that a layer of brittle Mo-carbide formed on the substrates of both the uncoated Mo-41Re and the uncoated Mo-47.5Re, subsequent to the C/C or the PyC/SiC processing. Both the R512E and the MoSi2(Ge) coatings were effective in preventing not only the diffusion of C into the Mo-Re substrate, but also the formation of the Mo-carbides. However, none of the coatings were effective at preventing both C and Si diffusion without some degradation of the substrate.
Document ID
20020021652
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Glass, David E.
(NASA Langley Research Center Hampton, VA United States)
Shenoy, Ravi N.
(Lockheed Martin Engineering and Sciences Co. Hampton, VA United States)
Wang, Zeng-Mei
(Chromealloy Gas Turbine Corp. Orangeburg, NJ United States)
Halbig, Michael C.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 2001
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:211264
NASA/TM-2001-211264
L-18116
Report Number: NAS 1.15:211264
Report Number: NASA/TM-2001-211264
Report Number: L-18116
Funding Number(s)
PROJECT: RTOP 242-33-03-20
CONTRACT_GRANT: NAS1-96014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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