C19010 Copper vs. 60Cr-40Ni Alloy
C19010 copper belongs to the copper alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. There are 19 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.
For each property being compared, the top bar is C19010 copper and the bottom bar is 60Cr-40Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 120 | |
220 |
Poisson's Ratio | 0.34 | |
0.25 |
Shear Modulus, GPa | 43 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 330 to 640 | |
870 |
Tensile Strength: Yield (Proof), MPa | 260 to 620 | |
660 |
Thermal Properties
Latent Heat of Fusion, J/g | 210 | |
370 |
Specific Heat Capacity, J/kg-K | 390 | |
490 |
Thermal Expansion, µm/m-K | 17 | |
16 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 31 | |
49 |
Density, g/cm3 | 8.9 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 2.7 | |
7.4 |
Embodied Energy, MJ/kg | 42 | |
110 |
Embodied Water, L/kg | 310 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 290 to 1680 | |
1000 |
Stiffness to Weight: Axial, points | 7.3 | |
16 |
Stiffness to Weight: Bending, points | 18 | |
26 |
Strength to Weight: Axial, points | 10 to 20 | |
31 |
Strength to Weight: Bending, points | 12 to 18 | |
26 |
Thermal Shock Resistance, points | 12 to 23 | |
18 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.25 |
Carbon (C), % | 0 | |
0 to 0.1 |
Chromium (Cr), % | 0 | |
58 to 62 |
Copper (Cu), % | 97.3 to 99.04 | |
0 |
Iron (Fe), % | 0 | |
0 to 1.0 |
Manganese (Mn), % | 0 | |
0 to 0.3 |
Nickel (Ni), % | 0.8 to 1.8 | |
34.5 to 42 |
Nitrogen (N), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0.010 to 0.050 | |
0 to 0.020 |
Silicon (Si), % | 0.15 to 0.35 | |
0 to 1.0 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Titanium (Ti), % | 0 | |
0 to 0.5 |
Residuals, % | 0 to 0.5 | |
0 |