6005A Aluminum vs. C17000 Copper
6005A aluminum belongs to the aluminum alloys classification, while C17000 copper belongs to the copper 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 6005A aluminum and the bottom bar is C17000 copper.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 120 |
| Elongation at Break, % | 8.6 to 17 | |
| 1.1 to 31 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 45 |
| Shear Strength, MPa | 120 to 180 | |
| 320 to 750 |
| Tensile Strength: Ultimate (UTS), MPa | 190 to 300 | |
| 490 to 1310 |
| Tensile Strength: Yield (Proof), MPa | 100 to 270 | |
| 160 to 1140 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 230 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 270 |
| Melting Completion (Liquidus), °C | 650 | |
| 980 |
| Melting Onset (Solidus), °C | 600 | |
| 870 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 390 |
| Thermal Conductivity, W/m-K | 180 to 190 | |
| 110 |
| Thermal Expansion, µm/m-K | 23 | |
| 17 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 47 to 50 | |
| 22 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 150 to 170 | |
| 22 |
Otherwise Unclassified Properties
| Density, g/cm3 | 2.7 | |
| 8.8 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 8.7 |
| Embodied Energy, MJ/kg | 150 | |
| 140 |
| Embodied Water, L/kg | 1180 | |
| 310 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 24 to 29 | |
| 4.2 to 390 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 76 to 530 | |
| 110 to 5420 |
| Stiffness to Weight: Axial, points | 14 | |
| 7.6 |
| Stiffness to Weight: Bending, points | 50 | |
| 19 |
| Strength to Weight: Axial, points | 20 to 30 | |
| 15 to 41 |
| Strength to Weight: Bending, points | 27 to 36 | |
| 16 to 30 |
| Thermal Diffusivity, mm2/s | 72 to 79 | |
| 32 |
| Thermal Shock Resistance, points | 8.6 to 13 | |
| 17 to 45 |
Alloy Composition
| Aluminum (Al), % | 96.5 to 99.1 | |
| 0 to 0.2 |
| Beryllium (Be), % | 0 | |
| 1.6 to 1.8 |
| Chromium (Cr), % | 0 to 0.3 | |
| 0 |
| Copper (Cu), % | 0 to 0.3 | |
| 96.3 to 98.2 |
| Iron (Fe), % | 0 to 0.35 | |
| 0 to 0.4 |
| Magnesium (Mg), % | 0.4 to 0.7 | |
| 0 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 0.2 to 0.6 |
| Silicon (Si), % | 0.5 to 0.9 | |
| 0 to 0.2 |
| Titanium (Ti), % | 0 to 0.1 | |
| 0 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.5 |