C55181 Copper vs. N06230 Nickel
C55181 copper belongs to the copper alloys classification, while N06230 nickel belongs to the nickel alloys. There are 20 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 C55181 copper and the bottom bar is N06230 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
210 |
Poisson's Ratio | 0.34 | |
0.28 |
Shear Modulus, GPa | 40 | |
83 |
Tensile Strength: Ultimate (UTS), MPa | 200 | |
620 to 840 |
Thermal Properties
Latent Heat of Fusion, J/g | 190 | |
310 |
Maximum Temperature: Mechanical, °C | 200 | |
990 |
Melting Completion (Liquidus), °C | 790 | |
1370 |
Melting Onset (Solidus), °C | 710 | |
1300 |
Specific Heat Capacity, J/kg-K | 410 | |
420 |
Thermal Expansion, µm/m-K | 16 | |
13 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 28 | |
85 |
Density, g/cm3 | 8.5 | |
9.5 |
Embodied Carbon, kg CO2/kg material | 2.4 | |
11 |
Embodied Energy, MJ/kg | 38 | |
160 |
Embodied Water, L/kg | 290 | |
290 |
Common Calculations
Stiffness to Weight: Axial, points | 7.0 | |
12 |
Stiffness to Weight: Bending, points | 19 | |
21 |
Strength to Weight: Axial, points | 6.5 | |
18 to 25 |
Strength to Weight: Bending, points | 8.9 | |
17 to 21 |
Thermal Shock Resistance, points | 8.2 | |
17 to 23 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.2 to 0.5 |
Boron (B), % | 0 | |
0 to 0.015 |
Carbon (C), % | 0 | |
0.050 to 0.15 |
Chromium (Cr), % | 0 | |
20 to 24 |
Cobalt (Co), % | 0 | |
0 to 5.0 |
Copper (Cu), % | 92.4 to 93 | |
0 |
Iron (Fe), % | 0 | |
0 to 3.0 |
Lanthanum (La), % | 0 | |
0.0050 to 0.050 |
Manganese (Mn), % | 0 | |
0.3 to 1.0 |
Molybdenum (Mo), % | 0 | |
1.0 to 3.0 |
Nickel (Ni), % | 0 | |
47.5 to 65.2 |
Phosphorus (P), % | 7.0 to 7.5 | |
0 to 0.030 |
Silicon (Si), % | 0 | |
0.25 to 0.75 |
Sulfur (S), % | 0 | |
0 to 0.015 |
Tungsten (W), % | 0 | |
13 to 15 |
Residuals, % | 0 to 0.15 | |
0 |