6063 Aluminum vs. EN-MC21110 Magnesium
6063 aluminum belongs to the aluminum alloys classification, while EN-MC21110 magnesium belongs to the magnesium alloys. 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 6063 aluminum and the bottom bar is EN-MC21110 magnesium.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 25 to 95 | |
| 58 to 63 |
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 46 |
| Elongation at Break, % | 7.3 to 21 | |
| 2.8 to 6.7 |
| Fatigue Strength, MPa | 39 to 95 | |
| 75 to 78 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 18 |
| Shear Strength, MPa | 70 to 190 | |
| 120 to 160 |
| Tensile Strength: Ultimate (UTS), MPa | 110 to 300 | |
| 200 to 270 |
| Tensile Strength: Yield (Proof), MPa | 49 to 270 | |
| 100 to 120 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 350 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 130 |
| Melting Completion (Liquidus), °C | 650 | |
| 600 |
| Melting Onset (Solidus), °C | 620 | |
| 500 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 990 |
| Thermal Conductivity, W/m-K | 190 to 220 | |
| 80 |
| Thermal Expansion, µm/m-K | 23 | |
| 26 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 49 to 58 | |
| 12 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 160 to 190 | |
| 61 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 12 |
| Density, g/cm3 | 2.7 | |
| 1.7 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 23 |
| Embodied Energy, MJ/kg | 150 | |
| 160 |
| Embodied Water, L/kg | 1190 | |
| 990 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 13 to 27 | |
| 4.9 to 14 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 18 to 540 | |
| 120 to 150 |
| Stiffness to Weight: Axial, points | 14 | |
| 15 |
| Stiffness to Weight: Bending, points | 50 | |
| 69 |
| Strength to Weight: Axial, points | 11 to 31 | |
| 33 to 44 |
| Strength to Weight: Bending, points | 18 to 37 | |
| 45 to 54 |
| Thermal Diffusivity, mm2/s | 79 to 89 | |
| 47 |
| Thermal Shock Resistance, points | 4.8 to 13 | |
| 12 to 16 |
Alloy Composition
| Aluminum (Al), % | 97.5 to 99.4 | |
| 7.0 to 8.7 |
| Chromium (Cr), % | 0 to 0.1 | |
| 0 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 to 0.030 |
| Iron (Fe), % | 0 to 0.35 | |
| 0 to 0.0050 |
| Magnesium (Mg), % | 0.45 to 0.9 | |
| 89.6 to 92.6 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0.1 to 0.35 |
| Nickel (Ni), % | 0 | |
| 0 to 0.0020 |
| Silicon (Si), % | 0.2 to 0.6 | |
| 0 to 0.2 |
| Titanium (Ti), % | 0 to 0.1 | |
| 0 |
| Zinc (Zn), % | 0 to 0.1 | |
| 0.35 to 1.0 |
| Residuals, % | 0 | |
| 0 to 0.010 |