60Cr-40Ni Alloy vs. C63200 Bronze
60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while C63200 bronze belongs to the copper alloys. There are 19 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.
For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is C63200 bronze.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 220 | |
| 120 |
| Poisson's Ratio | 0.25 | |
| 0.34 |
| Shear Modulus, GPa | 87 | |
| 44 |
| Tensile Strength: Ultimate (UTS), MPa | 870 | |
| 640 to 710 |
| Tensile Strength: Yield (Proof), MPa | 660 | |
| 310 to 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 370 | |
| 230 |
| Specific Heat Capacity, J/kg-K | 490 | |
| 440 |
| Thermal Expansion, µm/m-K | 16 | |
| 18 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 49 | |
| 29 |
| Density, g/cm3 | 7.8 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 7.4 | |
| 3.4 |
| Embodied Energy, MJ/kg | 110 | |
| 55 |
| Embodied Water, L/kg | 380 | |
| 380 |
Common Calculations
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1000 | |
| 400 to 510 |
| Stiffness to Weight: Axial, points | 16 | |
| 7.9 |
| Stiffness to Weight: Bending, points | 26 | |
| 20 |
| Strength to Weight: Axial, points | 31 | |
| 21 to 24 |
| Strength to Weight: Bending, points | 26 | |
| 20 to 21 |
| Thermal Shock Resistance, points | 18 | |
| 22 to 24 |
Alloy Composition
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| Aluminum (Al), % | 0 to 0.25 | |
| 8.7 to 9.5 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 58 to 62 | |
| 0 |
| Copper (Cu), % | 0 | |
| 78.8 to 82.6 |
| Iron (Fe), % | 0 to 1.0 | |
| 3.5 to 4.3 |
| Lead (Pb), % | 0 | |
| 0 to 0.020 |
| Manganese (Mn), % | 0 to 0.3 | |
| 1.2 to 2.0 |
| Nickel (Ni), % | 34.5 to 42 | |
| 4.0 to 4.8 |
| Nitrogen (N), % | 0 to 0.3 | |
| 0 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.1 |
| Sulfur (S), % | 0 to 0.020 | |
| 0 |
| Titanium (Ti), % | 0 to 0.5 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.5 |