C17200 Copper vs. 60Cr-40Ni Alloy
C17200 copper belongs to the copper alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. There are 18 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 C17200 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 | 0.33 | |
0.25 |
Shear Modulus, GPa | 45 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 480 to 1380 | |
870 |
Tensile Strength: Yield (Proof), MPa | 160 to 1250 | |
660 |
Thermal Properties
Latent Heat of Fusion, J/g | 230 | |
370 |
Specific Heat Capacity, J/kg-K | 390 | |
490 |
Thermal Expansion, µm/m-K | 18 | |
16 |
Otherwise Unclassified Properties
Density, g/cm3 | 8.8 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 9.4 | |
7.4 |
Embodied Energy, MJ/kg | 150 | |
110 |
Embodied Water, L/kg | 310 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 5720 | |
1000 |
Stiffness to Weight: Axial, points | 7.6 | |
16 |
Stiffness to Weight: Bending, points | 19 | |
26 |
Strength to Weight: Axial, points | 15 to 44 | |
31 |
Strength to Weight: Bending, points | 16 to 31 | |
26 |
Thermal Shock Resistance, points | 16 to 46 | |
18 |
Alloy Composition
Aluminum (Al), % | 0 to 0.2 | |
0 to 0.25 |
Beryllium (Be), % | 1.8 to 2.0 | |
0 |
Carbon (C), % | 0 | |
0 to 0.1 |
Chromium (Cr), % | 0 | |
58 to 62 |
Copper (Cu), % | 96.1 to 98 | |
0 |
Iron (Fe), % | 0 to 0.4 | |
0 to 1.0 |
Manganese (Mn), % | 0 | |
0 to 0.3 |
Nickel (Ni), % | 0.2 to 0.6 | |
34.5 to 42 |
Nitrogen (N), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 | |
0 to 0.020 |
Silicon (Si), % | 0 to 0.2 | |
0 to 1.0 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Titanium (Ti), % | 0 | |
0 to 0.5 |
Residuals, % | 0 to 0.5 | |
0 |