5086 Aluminum vs. 201.0 Aluminum
Both 5086 aluminum and 201.0 aluminum are aluminum alloys. They have a moderately 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 (4, in this case) are not shown.
For each property being compared, the top bar is 5086 aluminum and the bottom bar is 201.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 65 to 100 | |
| 95 to 140 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 71 |
| Elongation at Break, % | 1.7 to 20 | |
| 4.4 to 20 |
| Fatigue Strength, MPa | 88 to 180 | |
| 120 to 150 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 27 |
| Shear Strength, MPa | 160 to 230 | |
| 290 |
| Tensile Strength: Ultimate (UTS), MPa | 270 to 390 | |
| 370 to 470 |
| Tensile Strength: Yield (Proof), MPa | 110 to 320 | |
| 220 to 400 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 170 |
| Melting Completion (Liquidus), °C | 640 | |
| 650 |
| Melting Onset (Solidus), °C | 590 | |
| 570 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 870 |
| Thermal Conductivity, W/m-K | 130 | |
| 120 |
| Thermal Expansion, µm/m-K | 24 | |
| 19 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 31 | |
| 30 to 33 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 100 | |
| 87 to 97 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 38 |
| Calomel Potential, mV | -760 | |
| -670 |
| Density, g/cm3 | 2.7 | |
| 3.1 |
| Embodied Carbon, kg CO2/kg material | 8.8 | |
| 8.7 |
| Embodied Energy, MJ/kg | 150 | |
| 160 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 5.8 to 42 | |
| 19 to 63 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 86 to 770 | |
| 330 to 1160 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 45 |
| Strength to Weight: Axial, points | 28 to 40 | |
| 33 to 42 |
| Strength to Weight: Bending, points | 34 to 44 | |
| 37 to 44 |
| Thermal Diffusivity, mm2/s | 52 | |
| 45 |
| Thermal Shock Resistance, points | 12 to 17 | |
| 19 to 25 |
Alloy Composition
| Aluminum (Al), % | 93 to 96.3 | |
| 92.1 to 95.1 |
| Chromium (Cr), % | 0.050 to 0.25 | |
| 0 |
| Copper (Cu), % | 0 to 0.1 | |
| 4.0 to 5.2 |
| Iron (Fe), % | 0 to 0.5 | |
| 0 to 0.15 |
| Magnesium (Mg), % | 3.5 to 4.5 | |
| 0.15 to 0.55 |
| Manganese (Mn), % | 0.2 to 0.7 | |
| 0.2 to 0.5 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.1 |
| Silver (Ag), % | 0 | |
| 0.4 to 1.0 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0.15 to 0.35 |
| Zinc (Zn), % | 0 to 0.25 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.1 |