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ATI Allvac® Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age

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® Rene 41® Nickel Superalloy, Heat Treatment: 1079°C (1975°F) + Age.pdf
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Material Notes:
Data provided by Allvac.Applications: Jet and rocket engines, torque rings, afterburners, and hardware; space shuttle turbo pumps seals.
Physical Properties Metric English Comments
Density 8.24 g/cc
0.298 lb/in³
Mechanical Properties Metric English Comments
Hardness, Brinell 334
334
Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop 363
363
Estimated from Rockwell C value.
Hardness, Rockwell C 36
36
Hardness, Vickers 349
349
Estimated from Rockwell C value.
Tensile Strength, Ultimate 1241 MPa
180000 psi
Tensile Strength, Yield 793 MPa

@Strain 0.200 %
115000 psi

@Strain 0.200 %
Elongation at Break 20 %
20 %
Reduction of Area 25 %
25 %
Component Elements Properties Metric English Comments
Aluminum, Al 1.6 %
1.6 %
Boron, B 0.0070 %
0.0070 %
Carbon, C 0.060 %
0.060 %
Chromium, Cr 19 %
19 %
Cobalt, Co 11 %
11 %
Iron, Fe 3.0 %
3.0 %
Molybdenum, Mo 9.75 %
9.75 %
Nickel, Ni 52 %
52 %
as balance
Titanium, Ti 3.15 %
3.15 %
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