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Creep rupture behavior of Stirling engine materialsThe automotive Stirling engine, being investigated jointly by the Department of Energy and NASA Lewis as an alternate to the internal combustion engine, uses high-pressure hydrogen as the working fluid. The long-term effects of hydrogen on the high temperature strength properties of materials is relatively unknown. This is especially true for the newly developed low-cost iron base alloy NASAUT 4G-A1. This iron-base alloy when tested in air has creep-rupture strengths in the directionally solidified condition comparable to the cobalt base alloy HS-31. The equiaxed (investment cast) NASAUT 4G-A1 has superior creep-rupture to the equiaxed iron-base alloy XF-818 both in air and 15 MPa hydrogen.
Document ID
19860005910
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Titran, R. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Scheuerman, C. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Stephens, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Subject Category
Metallic Materials
Report/Patent Number
DOE/NASA/51044-37
NASA-TM-87209
E-2846
NAS 1.15:87209
Report Number: DOE/NASA/51044-37
Report Number: NASA-TM-87209
Report Number: E-2846
Report Number: NAS 1.15:87209
Meeting Information
Meeting: Advanced Technology Development Contractors Coordination Meeting
Location: Dearborn, MI
Country: United States
Start Date: October 21, 1985
End Date: October 24, 1985
Sponsors: DOE
Accession Number
86N15380
Funding Number(s)
PROJECT: RTOP 778-35-13
CONTRACT_GRANT: DE-AI01-77CS-51044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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