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Nickel base alloy with improved stress rupture propertiesNickel base superalloy with improved stress rupture properties is used for jet aircraft turbine blades. This alloy is capable of maintaining its strength and its creep, oxidation, and thermal fatigue resistance at high temperature.
Document ID
19680000344
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Collins, H. E.
Quigg, R. J.
Date Acquired
August 4, 2013
Publication Date
September 1, 1968
Subject Category
Materials
Report/Patent Number
LEW-10283
Accession Number
68B10344
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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