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60Cr-40Ni Alloy vs. ASTM B522 Class I

Both 60Cr-40Ni alloy and ASTM B522 class I are otherwise unclassified metals. There are 15 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is ASTM B522 class I.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
96
Poisson's Ratio 0.25
0.41
Shear Modulus, GPa 87
34
Tensile Strength: Ultimate (UTS), MPa 870
280 to 490
Tensile Strength: Yield (Proof), MPa 660
120 to 210

Thermal Properties

Latent Heat of Fusion, J/g 370
77
Specific Heat Capacity, J/kg-K 490
160
Thermal Expansion, µm/m-K 16
15

Otherwise Unclassified Properties

Density, g/cm3 7.8
17

Common Calculations

Resilience: Unit (Modulus of Resilience), kJ/m3 1000
75 to 230
Stiffness to Weight: Axial, points 16
3.1
Stiffness to Weight: Bending, points 26
8.9
Strength to Weight: Axial, points 31
4.4 to 7.8
Strength to Weight: Bending, points 26
5.5 to 8.0
Thermal Shock Resistance, points 18
13 to 24

Alloy Composition

Aluminum (Al), % 0 to 0.25
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 58 to 62
0
Gold (Au), % 0
68 to 70
Iron (Fe), % 0 to 1.0
0
Manganese (Mn), % 0 to 0.3
0
Nickel (Ni), % 34.5 to 42
0
Nitrogen (N), % 0 to 0.3
0
Phosphorus (P), % 0 to 0.020
0
Platinum (Pt), % 0
5.0 to 7.0
Silicon (Si), % 0 to 1.0
0
Silver (Ag), % 0
23.5 to 26.5
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0 to 0.5
0
Residuals, % 0
0 to 0.35