359.0 Aluminum vs. C17200 Copper
359.0 aluminum belongs to the aluminum alloys classification, while C17200 copper belongs to the copper alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, 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 359.0 aluminum and the bottom bar is C17200 copper.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 71 | |
| 120 |
| Elongation at Break, % | 3.8 to 4.9 | |
| 1.1 to 37 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 27 | |
| 45 |
| Shear Strength, MPa | 220 to 230 | |
| 330 to 780 |
| Tensile Strength: Ultimate (UTS), MPa | 340 to 350 | |
| 480 to 1380 |
| Tensile Strength: Yield (Proof), MPa | 250 to 280 | |
| 160 to 1250 |
Thermal Properties
| Latent Heat of Fusion, J/g | 530 | |
| 230 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 280 |
| Melting Completion (Liquidus), °C | 600 | |
| 980 |
| Melting Onset (Solidus), °C | 570 | |
| 870 |
| Specific Heat Capacity, J/kg-K | 910 | |
| 390 |
| Thermal Conductivity, W/m-K | 140 | |
| 110 |
| Thermal Expansion, µm/m-K | 21 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 35 | |
| 22 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 120 | |
| 23 |
Otherwise Unclassified Properties
| Density, g/cm3 | 2.6 | |
| 8.8 |
| Embodied Carbon, kg CO2/kg material | 8.0 | |
| 9.4 |
| Embodied Energy, MJ/kg | 150 | |
| 150 |
| Embodied Water, L/kg | 1090 | |
| 310 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 12 to 15 | |
| 4.2 to 500 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 450 to 540 | |
| 110 to 5720 |
| Stiffness to Weight: Axial, points | 15 | |
| 7.6 |
| Stiffness to Weight: Bending, points | 54 | |
| 19 |
| Strength to Weight: Axial, points | 37 to 38 | |
| 15 to 44 |
| Strength to Weight: Bending, points | 42 to 43 | |
| 16 to 31 |
| Thermal Diffusivity, mm2/s | 59 | |
| 31 |
| Thermal Shock Resistance, points | 16 to 17 | |
| 16 to 46 |
Alloy Composition
| Aluminum (Al), % | 88.9 to 91 | |
| 0 to 0.2 |
| Beryllium (Be), % | 0 | |
| 1.8 to 2.0 |
| Copper (Cu), % | 0 to 0.2 | |
| 96.1 to 98 |
| Iron (Fe), % | 0 to 0.2 | |
| 0 to 0.4 |
| Magnesium (Mg), % | 0.5 to 0.7 | |
| 0 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 0.2 to 0.6 |
| Silicon (Si), % | 8.5 to 9.5 | |
| 0 to 0.2 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.5 |