C19800 Copper vs. 60Cr-40Ni Alloy
C19800 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 C19800 copper and the bottom bar is 60Cr-40Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
220 |
Poisson's Ratio | 0.34 | |
0.25 |
Shear Modulus, GPa | 43 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 430 to 550 | |
870 |
Tensile Strength: Yield (Proof), MPa | 420 to 550 | |
660 |
Thermal Properties
Latent Heat of Fusion, J/g | 210 | |
370 |
Specific Heat Capacity, J/kg-K | 390 | |
490 |
Thermal Expansion, µm/m-K | 18 | |
16 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 30 | |
49 |
Density, g/cm3 | 8.9 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 2.8 | |
7.4 |
Embodied Energy, MJ/kg | 43 | |
110 |
Embodied Water, L/kg | 320 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 770 to 1320 | |
1000 |
Stiffness to Weight: Axial, points | 7.2 | |
16 |
Stiffness to Weight: Bending, points | 18 | |
26 |
Strength to Weight: Axial, points | 14 to 17 | |
31 |
Strength to Weight: Bending, points | 14 to 17 | |
26 |
Thermal Shock Resistance, points | 15 to 20 | |
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), % | 95.7 to 99.47 | |
0 |
Iron (Fe), % | 0.020 to 0.5 | |
0 to 1.0 |
Magnesium (Mg), % | 0.1 to 1.0 | |
0 |
Manganese (Mn), % | 0 | |
0 to 0.3 |
Nickel (Ni), % | 0 | |
34.5 to 42 |
Nitrogen (N), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0.010 to 0.1 | |
0 to 0.020 |
Silicon (Si), % | 0 | |
0 to 1.0 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Tin (Sn), % | 0.1 to 1.0 | |
0 |
Titanium (Ti), % | 0 | |
0 to 0.5 |
Zinc (Zn), % | 0.3 to 1.5 | |
0 |
Residuals, % | 0 to 0.2 | |
0 |