60Cr-40Ni Alloy vs. R31537 Cobalt
60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while R31537 cobalt belongs to the cobalt alloys. They have a modest 30% of their average alloy composition in common, which, by itself, doesn't mean much. There are 18 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.
For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is R31537 cobalt.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 220 | |
220 |
Poisson's Ratio | 0.25 | |
0.29 |
Shear Modulus, GPa | 87 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 870 | |
1000 to 1340 |
Tensile Strength: Yield (Proof), MPa | 660 | |
590 to 940 |
Thermal Properties
Latent Heat of Fusion, J/g | 370 | |
320 |
Specific Heat Capacity, J/kg-K | 490 | |
450 |
Thermal Expansion, µm/m-K | 16 | |
13 |
Otherwise Unclassified Properties
Density, g/cm3 | 7.8 | |
8.4 |
Embodied Carbon, kg CO2/kg material | 7.4 | |
8.1 |
Embodied Energy, MJ/kg | 110 | |
110 |
Embodied Water, L/kg | 380 | |
530 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1000 | |
780 to 1990 |
Stiffness to Weight: Axial, points | 16 | |
15 |
Stiffness to Weight: Bending, points | 26 | |
24 |
Strength to Weight: Axial, points | 31 | |
33 to 44 |
Strength to Weight: Bending, points | 26 | |
26 to 32 |
Thermal Shock Resistance, points | 18 | |
24 to 32 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.14 |
Chromium (Cr), % | 58 to 62 | |
26 to 30 |
Cobalt (Co), % | 0 | |
58.9 to 69 |
Iron (Fe), % | 0 to 1.0 | |
0 to 0.75 |
Manganese (Mn), % | 0 to 0.3 | |
0 to 1.0 |
Molybdenum (Mo), % | 0 | |
5.0 to 7.0 |
Nickel (Ni), % | 34.5 to 42 | |
0 to 1.0 |
Nitrogen (N), % | 0 to 0.3 | |
0 to 0.25 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
0 to 1.0 |
Sulfur (S), % | 0 to 0.020 | |
0 |
Titanium (Ti), % | 0 to 0.5 | |
0 |