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Effects of high temperature brazing and thermal cycling on mechanical properties of Hastelloy X.Data are presented on the effects of brazing alloy, brazing operation, thermal cycling, and combinations of these on the yield strength, elongation, ultimate tensile strength, and fatigue life of thin gage Hastelloy X. These data show that brazing with a Ni-Pd-Au alloy at 1461 K resulted in reductions of 35 percent in yield strength and elongation, 6 percent in ultimate tensile strength, and 18 percent in fatigue limit of Hastelloy X, as compared with as-received material. Subsequent exposure to 200 thermal cycles between 533 K and 1144 K after brazing caused further losses of 4 percent in yield strength, 8 percent in ultimate tensile strength, and 6 percent in fatigue limit.
Document ID
19730004802
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dicus, D. L.
(NASA Langley Research Center Hampton, VA, United States)
Buckley, J. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Materials, Metallic
Report/Patent Number
L-8561
NASA-TM-X-2704
Report Number: L-8561
Report Number: NASA-TM-X-2704
Accession Number
73N13529
Funding Number(s)
PROJECT: RTOP 502-21-20-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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