R30001 Cobalt vs. 60Cr-40Ni Alloy
R30001 cobalt belongs to the cobalt alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. They have a modest 33% of their average alloy composition in common, which, by itself, doesn't mean much. There are 16 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 R30001 cobalt and the bottom bar is 60Cr-40Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 220 | |
| 220 |
| Poisson's Ratio | 0.28 | |
| 0.25 |
| Shear Modulus, GPa | 86 | |
| 87 |
| Tensile Strength: Ultimate (UTS), MPa | 620 | |
| 870 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 370 |
| Specific Heat Capacity, J/kg-K | 430 | |
| 490 |
| Thermal Expansion, µm/m-K | 11 | |
| 16 |
Otherwise Unclassified Properties
| Density, g/cm3 | 9.0 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.9 | |
| 7.4 |
| Embodied Energy, MJ/kg | 130 | |
| 110 |
| Embodied Water, L/kg | 460 | |
| 380 |
Common Calculations
| Stiffness to Weight: Axial, points | 14 | |
| 16 |
| Stiffness to Weight: Bending, points | 22 | |
| 26 |
| Strength to Weight: Axial, points | 19 | |
| 31 |
| Strength to Weight: Bending, points | 18 | |
| 26 |
| Thermal Shock Resistance, points | 19 | |
| 18 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.25 |
| Carbon (C), % | 2.0 to 3.0 | |
| 0 to 0.1 |
| Chromium (Cr), % | 28 to 32 | |
| 58 to 62 |
| Cobalt (Co), % | 43 to 59 | |
| 0 |
| Iron (Fe), % | 0 to 3.0 | |
| 0 to 1.0 |
| Manganese (Mn), % | 0 | |
| 0 to 0.3 |
| Molybdenum (Mo), % | 0 to 1.0 | |
| 0 |
| Nickel (Ni), % | 0 to 3.0 | |
| 34.5 to 42 |
| Nitrogen (N), % | 0 | |
| 0 to 0.3 |
| Phosphorus (P), % | 0 | |
| 0 to 0.020 |
| Silicon (Si), % | 0 to 2.0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.020 |
| Titanium (Ti), % | 0 | |
| 0 to 0.5 |
| Tungsten (W), % | 11 to 13 | |
| 0 |