7108A Aluminum vs. C63000 Bronze
7108A aluminum belongs to the aluminum alloys classification, while C63000 bronze belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (1, 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 7108A aluminum and the bottom bar is C63000 bronze.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 120 |
| Elongation at Break, % | 11 to 13 | |
| 7.9 to 15 |
| Poisson's Ratio | 0.33 | |
| 0.34 |
| Shear Modulus, GPa | 26 | |
| 44 |
| Shear Strength, MPa | 210 | |
| 400 to 470 |
| Tensile Strength: Ultimate (UTS), MPa | 350 | |
| 660 to 790 |
| Tensile Strength: Yield (Proof), MPa | 290 to 300 | |
| 330 to 390 |
Thermal Properties
| Latent Heat of Fusion, J/g | 380 | |
| 230 |
| Maximum Temperature: Mechanical, °C | 210 | |
| 230 |
| Melting Completion (Liquidus), °C | 630 | |
| 1050 |
| Melting Onset (Solidus), °C | 520 | |
| 1040 |
| Specific Heat Capacity, J/kg-K | 870 | |
| 440 |
| Thermal Conductivity, W/m-K | 150 | |
| 39 |
| Thermal Expansion, µm/m-K | 24 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 36 | |
| 7.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 110 | |
| 7.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 29 |
| Density, g/cm3 | 2.9 | |
| 8.2 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 3.5 |
| Embodied Energy, MJ/kg | 150 | |
| 57 |
| Embodied Water, L/kg | 1150 | |
| 390 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 38 to 44 | |
| 47 to 82 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 610 to 640 | |
| 470 to 640 |
| Stiffness to Weight: Axial, points | 13 | |
| 7.9 |
| Stiffness to Weight: Bending, points | 47 | |
| 20 |
| Strength to Weight: Axial, points | 33 to 34 | |
| 22 to 26 |
| Strength to Weight: Bending, points | 38 | |
| 20 to 23 |
| Thermal Diffusivity, mm2/s | 59 | |
| 11 |
| Thermal Shock Resistance, points | 15 to 16 | |
| 23 to 27 |
Alloy Composition
| Aluminum (Al), % | 91.6 to 94.4 | |
| 9.0 to 11 |
| Chromium (Cr), % | 0 to 0.040 | |
| 0 |
| Copper (Cu), % | 0 to 0.050 | |
| 76.8 to 85 |
| Gallium (Ga), % | 0 to 0.030 | |
| 0 |
| Iron (Fe), % | 0 to 0.3 | |
| 2.0 to 4.0 |
| Magnesium (Mg), % | 0.7 to 1.5 | |
| 0 |
| Manganese (Mn), % | 0 to 0.050 | |
| 0 to 1.5 |
| Nickel (Ni), % | 0 | |
| 4.0 to 5.5 |
| Silicon (Si), % | 0 to 0.2 | |
| 0 to 0.25 |
| Tin (Sn), % | 0 | |
| 0 to 0.2 |
| Titanium (Ti), % | 0 to 0.030 | |
| 0 |
| Zinc (Zn), % | 4.8 to 5.8 | |
| 0 to 0.3 |
| Zirconium (Zr), % | 0.15 to 0.25 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.5 |