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Effects of Hydrogen on GRCop-84This report is a section of the final report on the GRCop-84 task of the Constellation Program and incorporates the results obtained between October 2000 and September 2005 when the program ended. GRCop-84 contains approximately 5.5 wt% Nb. Nb can react with H and embrittle easily. Previous work had indicated the thermodynamic possibility that Cr 2 Nb could react with H and form niobium hydrides in the presence of high pressure H such as seen in the Space Shuttle Main Engine. In this study, samples were charged with H and then tested in both high pressure H and He environments to determine if measurable differences existed which indicate that hydrogen embrittlement occurs in GRCop-84. Tensile, notched tensile, stress rupture and low cycle fatigue properties were surveyed. High pressure H environment stress rupture testing resulted in a lower reduction in area than a high pressure He environment, and the LCF lives at high strain ranges fall below the lower 95 percent confidence interval for the baseline data, but in general no significant differences were noted either between H and He environment tests or between hydrogen charged materials and the baseline, uncharged extruded GRCop-84 data sets. There was also no discernable evidence of the formation of hydrides or changes in fracture morphology indicating hydrogen embrittlement occurred.
Document ID
20060017836
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Ellis, David L.
(NASA Glenn Research Center Cleveland, OH, United States)
Hastings, Keith
(Jacobs Sverdrup Technology, Inc. Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
April 1, 2006
Subject Category
Metals And Metallic Materials
Report/Patent Number
NASA/TM-2006-214269
E-15555
Report Number: NASA/TM-2006-214269
Report Number: E-15555
Funding Number(s)
WBS: WBS 22-617-44-20
Distribution Limits
Public
Copyright
Public Use Permitted.
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