C99300 Copper vs. 6018 Aluminum
C99300 copper belongs to the copper alloys classification, while 6018 aluminum belongs to the aluminum alloys. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is C99300 copper and the bottom bar is 6018 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 120 | |
| 69 |
| Elongation at Break, % | 2.0 | |
| 9.0 to 9.1 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 46 | |
| 26 |
| Tensile Strength: Ultimate (UTS), MPa | 660 | |
| 290 to 300 |
| Tensile Strength: Yield (Proof), MPa | 380 | |
| 220 to 230 |
Thermal Properties
| Latent Heat of Fusion, J/g | 240 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 250 | |
| 160 |
| Melting Completion (Liquidus), °C | 1080 | |
| 640 |
| Melting Onset (Solidus), °C | 1070 | |
| 570 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 890 |
| Thermal Conductivity, W/m-K | 43 | |
| 170 |
| Thermal Expansion, µm/m-K | 17 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 9.0 | |
| 44 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 9.8 | |
| 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 35 | |
| 10 |
| Density, g/cm3 | 8.2 | |
| 2.9 |
| Embodied Carbon, kg CO2/kg material | 4.5 | |
| 8.2 |
| Embodied Energy, MJ/kg | 70 | |
| 150 |
| Embodied Water, L/kg | 400 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 11 | |
| 24 to 25 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 590 | |
| 360 to 380 |
| Stiffness to Weight: Axial, points | 8.3 | |
| 13 |
| Stiffness to Weight: Bending, points | 20 | |
| 48 |
| Strength to Weight: Axial, points | 22 | |
| 28 to 29 |
| Strength to Weight: Bending, points | 20 | |
| 34 to 35 |
| Thermal Diffusivity, mm2/s | 12 | |
| 65 |
| Thermal Shock Resistance, points | 22 | |
| 13 |
Alloy Composition
| Aluminum (Al), % | 10.7 to 11.5 | |
| 93.1 to 97.8 |
| Bismuth (Bi), % | 0 | |
| 0.4 to 0.7 |
| Chromium (Cr), % | 0 | |
| 0 to 0.1 |
| Cobalt (Co), % | 1.0 to 2.0 | |
| 0 |
| Copper (Cu), % | 68.6 to 74.4 | |
| 0.15 to 0.4 |
| Iron (Fe), % | 0.4 to 1.0 | |
| 0 to 0.7 |
| Lead (Pb), % | 0 to 0.020 | |
| 0.4 to 1.2 |
| Magnesium (Mg), % | 0 | |
| 0.6 to 1.2 |
| Manganese (Mn), % | 0 | |
| 0.3 to 0.8 |
| Nickel (Ni), % | 13.5 to 16.5 | |
| 0 |
| Silicon (Si), % | 0 to 0.020 | |
| 0.5 to 1.2 |
| Tin (Sn), % | 0 to 0.050 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.2 |
| Zinc (Zn), % | 0 | |
| 0 to 0.3 |
| Residuals, % | 0 | |
| 0 to 0.15 |