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Creep-rupture behavior of a developmental cast-iron-base alloy for use up to 800 deg CA promising iron-base cast alloy is being developed as part of the DOE/NASA Stirling Engine Systems Project under contract DEN 3-282 with the United Technologies Research Center. This report presents the results of a study at the Lewis Research Center of the alloy's creep-rupture properties. The alloy was tested under a variety of conditions and was found to exhibit the normal 3-stage creep response. The alloy compared favorably with others being used or under consideration for the automotive Stirling engine cylinder/regenerator housing.
Document ID
19870019208
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Titran, Robert H.
(NASA Lewis Research Center Cleveland, OH, United States)
Scheuermann, Coulson M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1987
Subject Category
Metallic Materials
Report/Patent Number
DOE/NASA/50112-70
NAS 1.15:100167
E-3346
NASA-TM-100167
Report Number: DOE/NASA/50112-70
Report Number: NAS 1.15:100167
Report Number: E-3346
Report Number: NASA-TM-100167
Accession Number
87N28641
Funding Number(s)
CONTRACT_GRANT: DE-AI01-85CE-50112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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