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ATI Allvac® M-252 Nickel Superalloy, Heat Treatment: 1177°C (2150°F) Anneal

Category Metal , Nonferrous Metal , Nickel Alloy , Superalloy
Manufacturer ATI Allvac
Trade Name
Port Shanghai port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF ATI Allvac® M-252 Nickel Superalloy, Heat Treatment: 1177°C (2150°F) Anneal.pdf
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Material Notes:
Applications: Turbine blades, fasteners, and high temperature bolting.Data provided by Allvac.
Physical Properties Metric English Comments
Density 8.24 g/cc
0.298 lb/in³
Mechanical Properties Metric English Comments
Hardness, Brinell 318
318
Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop 346
346
Estimated from Rockwell C value.
Hardness, Rockwell C 34
34
Hardness, Vickers 333
333
Estimated from Rockwell C value.
Tensile Strength, Ultimate 1379 MPa
200000 psi
Tensile Strength, Yield 345 MPa

@Strain 0.200 %
50000 psi

@Strain 0.200 %
Elongation at Break 50 %
50 %
Reduction of Area 50 %
50 %
Component Elements Properties Metric English Comments
Aluminum, Al 1.0 %
1.0 %
Boron, B 0.0070 %
0.0070 %
Carbon, C 0.015 %
0.015 %
Chromium, Cr 19 %
19 %
Cobalt, Co 10 %
10 %
Iron, Fe 2.5 %
2.5 %
Molybdenum, Mo 9.75 %
9.75 %
Nickel, Ni 55 %
55 %
as balance
Titanium, Ti 2.5 %
2.5 %
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