A206.0 Aluminum vs. 5021 Aluminum
Both A206.0 aluminum and 5021 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is A206.0 aluminum and the bottom bar is 5021 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 68 |
| Elongation at Break, % | 4.2 to 10 | |
| 1.1 to 3.4 |
| Fatigue Strength, MPa | 90 to 180 | |
| 85 to 110 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 26 |
| Shear Strength, MPa | 260 | |
| 170 |
| Tensile Strength: Ultimate (UTS), MPa | 390 to 440 | |
| 300 to 310 |
| Tensile Strength: Yield (Proof), MPa | 250 to 380 | |
| 240 to 270 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 180 |
| Melting Completion (Liquidus), °C | 670 | |
| 640 |
| Melting Onset (Solidus), °C | 550 | |
| 590 |
| Specific Heat Capacity, J/kg-K | 880 | |
| 900 |
| Thermal Conductivity, W/m-K | 130 | |
| 140 |
| Thermal Expansion, µm/m-K | 23 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 30 | |
| 35 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 90 | |
| 120 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 9.5 |
| Density, g/cm3 | 3.0 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 8.0 | |
| 8.6 |
| Embodied Energy, MJ/kg | 150 | |
| 150 |
| Embodied Water, L/kg | 1150 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 16 to 37 | |
| 3.1 to 10 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 440 to 1000 | |
| 440 to 550 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 46 | |
| 50 |
| Strength to Weight: Axial, points | 36 to 41 | |
| 30 to 32 |
| Strength to Weight: Bending, points | 39 to 43 | |
| 37 |
| Thermal Diffusivity, mm2/s | 48 | |
| 57 |
| Thermal Shock Resistance, points | 17 to 19 | |
| 13 to 14 |
Alloy Composition
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| Aluminum (Al), % | 93.9 to 95.7 | |
| 95.2 to 97.7 |
| Chromium (Cr), % | 0 | |
| 0 to 0.15 |
| Copper (Cu), % | 4.2 to 5.0 | |
| 0 to 0.15 |
| Iron (Fe), % | 0 to 0.1 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 to 0.15 | |
| 2.2 to 2.8 |
| Manganese (Mn), % | 0 to 0.2 | |
| 0.1 to 0.5 |
| Nickel (Ni), % | 0 to 0.050 | |
| 0 |
| Silicon (Si), % | 0 to 0.050 | |
| 0 to 0.4 |
| Tin (Sn), % | 0 to 0.050 | |
| 0 |
| Titanium (Ti), % | 0.15 to 0.3 | |
| 0 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0 to 0.15 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.15 |