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

Both ASTM B522 class I and 60Cr-40Ni alloy 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 ASTM B522 class I and the bottom bar is 60Cr-40Ni alloy.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

Density, g/cm3 17
7.8

Common Calculations

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

Alloy Composition

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