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Arc termination cracks in Inconel 718 and Incoloy 903The welding of the nickel base, heat resistant alloys that are used extensively for welded Shuttle engine components revealed solidification cracking characteristics at weld termination points. If not detected and removed, these crater cracks may cause costly component failure. To better understand this characteristic, welding termination techniques were studied and methods developed to eliminate crater cracks. It was determined that weld termination solidification cracking can be eliminated by controlled decrease of welding current, welding voltage, wire feed, and travel speed.
Document ID
19790002013
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bayless, E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Mccaig, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Poorman, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1978
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-78201
Report Number: NASA-TM-78201
Accession Number
79N10184
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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