Series of nickel-base alloys not requiring vacuum melting techniques and providing good stress-rupture and impact properties was developed for possible aircraft turbine blade or space applications; strongest composition displayed stress-rupture lives of 384 and 574 hr in as-cast and homogenized conditions, respectively, at 1800 F and 15,000 psi.
Exploratory investigation of advanced-temperature nickel-base alloys
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 4-13-59E
1959
39 pages
Report
Englisch
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High Temperature, high strength Nickel Base Alloys
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