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Master Bond adhesives

ATI Allvac® Nickelvac® N-90 Nickel Superalloy, Heat Treatment: 1066°C (1950°F) + Age
Categories: Metal; Nonferrous Metal; Nickel Alloy; Superalloy

Material Notes: Data provided by Allvac.

Applications: Turbine blades and other jet engine components. Valves for internal combustion engines.

Key Words: Allvac, an Allegheny Teledyne Company, UNS N07090; AMS 5829. SAE J 775
Vendors: Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494.

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Physical PropertiesMetricEnglishComments
Density 8.11 g/cc0.293 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 278278Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop 301301Estimated from Rockwell C value.
Hardness, Rockwell C 2828
Hardness, Vickers 292292Estimated from Rockwell C value.
Tensile Strength, Ultimate 1207 MPa175100 psi
Tensile Strength, Yield 517 MPa
@Strain 0.2 %
75000 psi
@Strain 0.2 %
Elongation at Break 30 %30 %
Reduction of Area 35 %35 %
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 1.4 %1.4 %
Carbon, C 0.065 %0.065 %
Chromium, Cr 19.5 %19.5 %
Cobalt, Co 18 %18 %
Iron, Fe 0.30 %0.30 %
Nickel, Ni 58 %58 %as balance
Titanium, Ti 2.4 %2.4 %

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to view all the property values for this datasheet as they were originally entered into MatWeb.

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