ISO-WD21150 Magnesium vs. 355.0 Aluminum
ISO-WD21150 magnesium belongs to the magnesium alloys classification, while 355.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is ISO-WD21150 magnesium and the bottom bar is 355.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 45 | |
| 71 |
| Elongation at Break, % | 5.7 to 11 | |
| 1.5 to 2.6 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 17 | |
| 27 |
| Shear Strength, MPa | 150 to 170 | |
| 150 to 240 |
| Tensile Strength: Ultimate (UTS), MPa | 240 to 290 | |
| 200 to 260 |
| Tensile Strength: Yield (Proof), MPa | 120 to 200 | |
| 150 to 190 |
Thermal Properties
| Latent Heat of Fusion, J/g | 350 | |
| 470 |
| Maximum Temperature: Mechanical, °C | 110 | |
| 180 |
| Melting Completion (Liquidus), °C | 600 | |
| 620 |
| Melting Onset (Solidus), °C | 550 | |
| 560 |
| Specific Heat Capacity, J/kg-K | 990 | |
| 890 |
| Thermal Conductivity, W/m-K | 100 | |
| 150 to 170 |
| Thermal Expansion, µm/m-K | 27 | |
| 22 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 19 | |
| 38 to 43 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 100 | |
| 120 to 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 9.5 |
| Density, g/cm3 | 1.7 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 23 | |
| 8.0 |
| Embodied Energy, MJ/kg | 160 | |
| 150 |
| Embodied Water, L/kg | 980 | |
| 1120 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 15 to 24 | |
| 2.7 to 5.9 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 160 to 460 | |
| 150 to 250 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 70 | |
| 51 |
| Strength to Weight: Axial, points | 40 to 48 | |
| 20 to 27 |
| Strength to Weight: Bending, points | 52 to 58 | |
| 28 to 33 |
| Thermal Diffusivity, mm2/s | 60 | |
| 60 to 69 |
| Thermal Shock Resistance, points | 15 to 17 | |
| 9.1 to 12 |
Alloy Composition
| Aluminum (Al), % | 2.4 to 3.6 | |
| 90.3 to 94.1 |
| Chromium (Cr), % | 0 | |
| 0 to 0.25 |
| Copper (Cu), % | 0 to 0.050 | |
| 1.0 to 1.5 |
| Iron (Fe), % | 0 to 0.0050 | |
| 0 to 0.6 |
| Magnesium (Mg), % | 94 to 97 | |
| 0.4 to 0.6 |
| Manganese (Mn), % | 0.15 to 0.4 | |
| 0 to 0.5 |
| Nickel (Ni), % | 0 to 0.0050 | |
| 0 |
| Silicon (Si), % | 0 to 0.1 | |
| 4.5 to 5.5 |
| Titanium (Ti), % | 0 | |
| 0 to 0.25 |
| Zinc (Zn), % | 0.5 to 1.5 | |
| 0 to 0.35 |
| Residuals, % | 0 | |
| 0 to 0.15 |