5383 Aluminum vs. A206.0 Aluminum
Both 5383 aluminum and A206.0 aluminum are aluminum alloys. They have a moderately high 94% 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 5383 aluminum and the bottom bar is A206.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 85 to 110 | |
| 100 to 110 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 70 |
| Elongation at Break, % | 6.7 to 15 | |
| 4.2 to 10 |
| Fatigue Strength, MPa | 130 to 200 | |
| 90 to 180 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 26 |
| Shear Strength, MPa | 190 to 220 | |
| 260 |
| Tensile Strength: Ultimate (UTS), MPa | 310 to 370 | |
| 390 to 440 |
| Tensile Strength: Yield (Proof), MPa | 150 to 310 | |
| 250 to 380 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 200 | |
| 170 |
| Melting Completion (Liquidus), °C | 650 | |
| 670 |
| Melting Onset (Solidus), °C | 540 | |
| 550 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 880 |
| Thermal Conductivity, W/m-K | 130 | |
| 130 |
| Thermal Expansion, µm/m-K | 24 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 29 | |
| 30 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 97 | |
| 90 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 11 |
| Density, g/cm3 | 2.7 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 9.0 | |
| 8.0 |
| Embodied Energy, MJ/kg | 160 | |
| 150 |
| Embodied Water, L/kg | 1170 | |
| 1150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 23 to 40 | |
| 16 to 37 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 to 690 | |
| 440 to 1000 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 46 |
| Strength to Weight: Axial, points | 32 to 38 | |
| 36 to 41 |
| Strength to Weight: Bending, points | 38 to 42 | |
| 39 to 43 |
| Thermal Diffusivity, mm2/s | 51 | |
| 48 |
| Thermal Shock Resistance, points | 14 to 16 | |
| 17 to 19 |
Alloy Composition
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| Aluminum (Al), % | 92 to 95.3 | |
| 93.9 to 95.7 |
| Chromium (Cr), % | 0 to 0.25 | |
| 0 |
| Copper (Cu), % | 0 to 0.2 | |
| 4.2 to 5.0 |
| Iron (Fe), % | 0 to 0.25 | |
| 0 to 0.1 |
| Magnesium (Mg), % | 4.0 to 5.2 | |
| 0 to 0.15 |
| Manganese (Mn), % | 0.7 to 1.0 | |
| 0 to 0.2 |
| Nickel (Ni), % | 0 | |
| 0 to 0.050 |
| Silicon (Si), % | 0 to 0.25 | |
| 0 to 0.050 |
| Tin (Sn), % | 0 | |
| 0 to 0.050 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0.15 to 0.3 |
| Zinc (Zn), % | 0 to 0.4 | |
| 0 to 0.1 |
| Zirconium (Zr), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.15 |