50Cr-50Ni Alloy vs. C19020 Copper
50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while C19020 copper belongs to the copper alloys. There are 18 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 50Cr-50Ni alloy and the bottom bar is C19020 copper.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 120 |
| Elongation at Break, % | 5.7 | |
| 2.3 to 5.7 |
| Poisson's Ratio | 0.26 | |
| 0.34 |
| Shear Modulus, GPa | 84 | |
| 44 |
| Tensile Strength: Ultimate (UTS), MPa | 620 | |
| 440 to 590 |
Thermal Properties
| Latent Heat of Fusion, J/g | 350 | |
| 210 |
| Specific Heat Capacity, J/kg-K | 490 | |
| 390 |
| Thermal Expansion, µm/m-K | 15 | |
| 17 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 50 | |
| 31 |
| Density, g/cm3 | 8.0 | |
| 8.9 |
| Embodied Carbon, kg CO2/kg material | 7.9 | |
| 2.8 |
| Embodied Energy, MJ/kg | 110 | |
| 44 |
| Embodied Water, L/kg | 350 | |
| 310 |
Common Calculations
| Stiffness to Weight: Axial, points | 15 | |
| 7.2 |
| Stiffness to Weight: Bending, points | 25 | |
| 18 |
| Strength to Weight: Axial, points | 21 | |
| 14 to 18 |
| Strength to Weight: Bending, points | 20 | |
| 14 to 18 |
| Thermal Shock Resistance, points | 14 | |
| 16 to 21 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.25 | |
| 0 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 48 to 52 | |
| 0 |
| Copper (Cu), % | 0 | |
| 95.7 to 99.19 |
| Iron (Fe), % | 0 to 1.0 | |
| 0 |
| Manganese (Mn), % | 0 to 0.3 | |
| 0 |
| Nickel (Ni), % | 44.5 to 52 | |
| 0.5 to 3.0 |
| Nitrogen (N), % | 0 to 0.3 | |
| 0 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0.010 to 0.2 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.020 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0.3 to 0.9 |
| Titanium (Ti), % | 0 to 0.5 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.2 |