60Cr-40Ni Alloy vs. C17500 Copper
60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while C17500 copper belongs to the copper alloys. There are 19 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 60Cr-40Ni alloy and the bottom bar is C17500 copper.
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 | |
45 |
Tensile Strength: Ultimate (UTS), MPa | 870 | |
310 to 860 |
Tensile Strength: Yield (Proof), MPa | 660 | |
170 to 760 |
Thermal Properties
Latent Heat of Fusion, J/g | 370 | |
220 |
Specific Heat Capacity, J/kg-K | 490 | |
390 |
Thermal Expansion, µm/m-K | 16 | |
18 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 49 | |
60 |
Density, g/cm3 | 7.8 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 7.4 | |
4.7 |
Embodied Energy, MJ/kg | 110 | |
73 |
Embodied Water, L/kg | 380 | |
320 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1000 | |
120 to 2390 |
Stiffness to Weight: Axial, points | 16 | |
7.5 |
Stiffness to Weight: Bending, points | 26 | |
18 |
Strength to Weight: Axial, points | 31 | |
9.7 to 27 |
Strength to Weight: Bending, points | 26 | |
11 to 23 |
Thermal Shock Resistance, points | 18 | |
11 to 29 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 to 0.2 |
Beryllium (Be), % | 0 | |
0.4 to 0.7 |
Carbon (C), % | 0 to 0.1 | |
0 |
Chromium (Cr), % | 58 to 62 | |
0 |
Cobalt (Co), % | 0 | |
2.4 to 2.7 |
Copper (Cu), % | 0 | |
95.6 to 97.2 |
Iron (Fe), % | 0 to 1.0 | |
0 to 0.1 |
Manganese (Mn), % | 0 to 0.3 | |
0 |
Nickel (Ni), % | 34.5 to 42 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
0 to 0.2 |
Sulfur (S), % | 0 to 0.020 | |
0 |
Titanium (Ti), % | 0 to 0.5 | |
0 |
Residuals, % | 0 | |
0 to 0.5 |