5050 Aluminum vs. A206.0 Aluminum
Both 5050 aluminum and A206.0 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common. There are 31 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 5050 aluminum and the bottom bar is A206.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 36 to 68 | |
| 100 to 110 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 70 |
| Elongation at Break, % | 1.7 to 22 | |
| 4.2 to 10 |
| Fatigue Strength, MPa | 45 to 100 | |
| 90 to 180 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 26 |
| Shear Strength, MPa | 91 to 140 | |
| 260 |
| Tensile Strength: Ultimate (UTS), MPa | 140 to 250 | |
| 390 to 440 |
| Tensile Strength: Yield (Proof), MPa | 50 to 210 | |
| 250 to 380 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 170 |
| Melting Completion (Liquidus), °C | 650 | |
| 670 |
| Melting Onset (Solidus), °C | 630 | |
| 550 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 880 |
| Thermal Conductivity, W/m-K | 190 | |
| 130 |
| Thermal Expansion, µm/m-K | 24 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 50 | |
| 30 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 170 | |
| 90 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 11 |
| Density, g/cm3 | 2.7 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 8.4 | |
| 8.0 |
| Embodied Energy, MJ/kg | 150 | |
| 150 |
| Embodied Water, L/kg | 1190 | |
| 1150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.1 to 24 | |
| 16 to 37 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 18 to 330 | |
| 440 to 1000 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 46 |
| Strength to Weight: Axial, points | 15 to 26 | |
| 36 to 41 |
| Strength to Weight: Bending, points | 22 to 33 | |
| 39 to 43 |
| Thermal Diffusivity, mm2/s | 79 | |
| 48 |
| Thermal Shock Resistance, points | 6.3 to 11 | |
| 17 to 19 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
| Aluminum (Al), % | 96.3 to 98.9 | |
| 93.9 to 95.7 |
| Chromium (Cr), % | 0 to 0.1 | |
| 0 |
| Copper (Cu), % | 0 to 0.2 | |
| 4.2 to 5.0 |
| Iron (Fe), % | 0 to 0.7 | |
| 0 to 0.1 |
| Magnesium (Mg), % | 1.1 to 1.8 | |
| 0 to 0.15 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0 to 0.2 |
| Nickel (Ni), % | 0 | |
| 0 to 0.050 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.050 |
| Tin (Sn), % | 0 | |
| 0 to 0.050 |
| Titanium (Ti), % | 0 | |
| 0.15 to 0.3 |
| Zinc (Zn), % | 0 to 0.25 | |
| 0 to 0.1 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.15 |