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Copper Alloy For High-Temperature UsesAlloy of Cu/8Cr/4Nb (numbers indicate parts by atom percent) improved over older high-temperature copper-based alloys in that it offers enhanced high temperature strength, resistance to creep, and ductility while retaining most of thermal conductivity of pure copper; in addition, alloy does not become embrittled upon exposure to hydrogen at temperatures as high as 705 degrees C. Designed for use in presence of high heat fluxes and active cooling; for example, in heat exchangers in advanced aircraft and spacecraft engines, and other high-temperature applications in which there is need for such material. High conductivity and hardness of alloy exploited in welding electrodes and in high-voltage and high-current switches and other applications in which wear poses design problem.
Document ID
19940000443
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Dreshfield, Robert L.
(NASA Lewis Research Center, Cleveland, OH.)
Ellis, David L.
(Case Western Reserve Univ.)
Michal, Gary
(Case Western Reserve Univ.)
Date Acquired
August 16, 2013
Publication Date
August 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 8
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LEW-15768
Accession Number
94B10443
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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