7050 Aluminum vs. C66200 Brass
7050 aluminum belongs to the aluminum alloys classification, while C66200 brass 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 7050 aluminum and the bottom bar is C66200 brass.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 110 |
| Elongation at Break, % | 2.2 to 12 | |
| 8.0 to 15 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 42 |
| Shear Strength, MPa | 280 to 330 | |
| 270 to 300 |
| Tensile Strength: Ultimate (UTS), MPa | 490 to 570 | |
| 450 to 520 |
| Tensile Strength: Yield (Proof), MPa | 390 to 500 | |
| 410 to 480 |
Thermal Properties
| Latent Heat of Fusion, J/g | 370 | |
| 200 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 180 |
| Melting Completion (Liquidus), °C | 630 | |
| 1070 |
| Melting Onset (Solidus), °C | 490 | |
| 1030 |
| Specific Heat Capacity, J/kg-K | 860 | |
| 390 |
| Thermal Conductivity, W/m-K | 140 | |
| 150 |
| Thermal Expansion, µm/m-K | 24 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 35 | |
| 35 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 100 | |
| 36 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 29 |
| Density, g/cm3 | 3.1 | |
| 8.7 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 2.7 |
| Embodied Energy, MJ/kg | 150 | |
| 43 |
| Embodied Water, L/kg | 1120 | |
| 320 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 10 to 55 | |
| 40 to 66 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1110 to 1760 | |
| 760 to 1030 |
| Stiffness to Weight: Axial, points | 13 | |
| 7.2 |
| Stiffness to Weight: Bending, points | 45 | |
| 19 |
| Strength to Weight: Axial, points | 45 to 51 | |
| 14 to 17 |
| Strength to Weight: Bending, points | 45 to 50 | |
| 15 to 16 |
| Thermal Diffusivity, mm2/s | 54 | |
| 45 |
| Thermal Shock Resistance, points | 21 to 25 | |
| 16 to 18 |
Alloy Composition
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| Aluminum (Al), % | 87.3 to 92.1 | |
| 0 |
| Chromium (Cr), % | 0 to 0.040 | |
| 0 |
| Copper (Cu), % | 2.0 to 2.6 | |
| 86.6 to 91 |
| Iron (Fe), % | 0 to 0.15 | |
| 0 to 0.050 |
| Lead (Pb), % | 0 | |
| 0 to 0.050 |
| Magnesium (Mg), % | 1.9 to 2.6 | |
| 0 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 0.3 to 1.0 |
| Phosphorus (P), % | 0 | |
| 0.050 to 0.2 |
| Silicon (Si), % | 0 to 0.12 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0.2 to 0.7 |
| Titanium (Ti), % | 0 to 0.060 | |
| 0 |
| Zinc (Zn), % | 5.7 to 6.7 | |
| 6.5 to 12.9 |
| Zirconium (Zr), % | 0.080 to 0.15 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.5 |