EN-MC21120 Magnesium vs. 5086 Aluminum
EN-MC21120 magnesium belongs to the magnesium alloys classification, while 5086 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is EN-MC21120 magnesium and the bottom bar is 5086 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 63 to 75 | |
| 65 to 100 |
| Elastic (Young's, Tensile) Modulus, GPa | 46 | |
| 68 |
| Elongation at Break, % | 2.2 to 6.7 | |
| 1.7 to 20 |
| Fatigue Strength, MPa | 84 to 96 | |
| 88 to 180 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 18 | |
| 26 |
| Shear Strength, MPa | 110 to 160 | |
| 160 to 230 |
| Tensile Strength: Ultimate (UTS), MPa | 200 to 270 | |
| 270 to 390 |
| Tensile Strength: Yield (Proof), MPa | 130 to 170 | |
| 110 to 320 |
Thermal Properties
| Latent Heat of Fusion, J/g | 350 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 130 | |
| 190 |
| Melting Completion (Liquidus), °C | 600 | |
| 640 |
| Melting Onset (Solidus), °C | 490 | |
| 590 |
| Specific Heat Capacity, J/kg-K | 990 | |
| 900 |
| Thermal Conductivity, W/m-K | 76 | |
| 130 |
| Thermal Expansion, µm/m-K | 26 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 11 | |
| 31 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 59 | |
| 100 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 9.5 |
| Density, g/cm3 | 1.7 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 22 | |
| 8.8 |
| Embodied Energy, MJ/kg | 160 | |
| 150 |
| Embodied Water, L/kg | 990 | |
| 1180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 5.0 to 15 | |
| 5.8 to 42 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 180 to 320 | |
| 86 to 770 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 69 | |
| 50 |
| Strength to Weight: Axial, points | 31 to 43 | |
| 28 to 40 |
| Strength to Weight: Bending, points | 43 to 53 | |
| 34 to 44 |
| Thermal Diffusivity, mm2/s | 44 | |
| 52 |
| Thermal Shock Resistance, points | 11 to 16 | |
| 12 to 17 |
Alloy Composition
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| Aluminum (Al), % | 8.3 to 9.7 | |
| 93 to 96.3 |
| Chromium (Cr), % | 0 | |
| 0.050 to 0.25 |
| Copper (Cu), % | 0 to 0.030 | |
| 0 to 0.1 |
| Iron (Fe), % | 0 to 0.0050 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 88.6 to 91.3 | |
| 3.5 to 4.5 |
| Manganese (Mn), % | 0.1 to 0.5 | |
| 0.2 to 0.7 |
| Nickel (Ni), % | 0 to 0.0020 | |
| 0 |
| Silicon (Si), % | 0 to 0.2 | |
| 0 to 0.4 |
| Titanium (Ti), % | 0 | |
| 0 to 0.15 |
| Zinc (Zn), % | 0.35 to 1.0 | |
| 0 to 0.25 |
| Residuals, % | 0 to 0.010 | |
| 0 to 0.15 |