ISO-WD21150 Magnesium vs. Grade 18 Titanium
ISO-WD21150 magnesium belongs to the magnesium alloys classification, while grade 18 titanium belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is ISO-WD21150 magnesium and the bottom bar is grade 18 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 45 | |
| 110 |
| Elongation at Break, % | 5.7 to 11 | |
| 11 to 17 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Shear Modulus, GPa | 17 | |
| 40 |
| Shear Strength, MPa | 150 to 170 | |
| 420 to 590 |
| Tensile Strength: Ultimate (UTS), MPa | 240 to 290 | |
| 690 to 980 |
| Tensile Strength: Yield (Proof), MPa | 120 to 200 | |
| 540 to 810 |
Thermal Properties
| Latent Heat of Fusion, J/g | 350 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 110 | |
| 330 |
| Melting Completion (Liquidus), °C | 600 | |
| 1640 |
| Melting Onset (Solidus), °C | 550 | |
| 1590 |
| Specific Heat Capacity, J/kg-K | 990 | |
| 550 |
| Thermal Conductivity, W/m-K | 100 | |
| 8.3 |
| Thermal Expansion, µm/m-K | 27 | |
| 9.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 19 | |
| 1.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 100 | |
| 2.7 |
Otherwise Unclassified Properties
| Density, g/cm3 | 1.7 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 23 | |
| 41 |
| Embodied Energy, MJ/kg | 160 | |
| 670 |
| Embodied Water, L/kg | 980 | |
| 270 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 15 to 24 | |
| 87 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 160 to 460 | |
| 1380 to 3110 |
| Stiffness to Weight: Axial, points | 15 | |
| 13 |
| Stiffness to Weight: Bending, points | 70 | |
| 35 |
| Strength to Weight: Axial, points | 40 to 48 | |
| 43 to 61 |
| Strength to Weight: Bending, points | 52 to 58 | |
| 39 to 49 |
| Thermal Diffusivity, mm2/s | 60 | |
| 3.4 |
| Thermal Shock Resistance, points | 15 to 17 | |
| 47 to 67 |
Alloy Composition
| Aluminum (Al), % | 2.4 to 3.6 | |
| 2.5 to 3.5 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Copper (Cu), % | 0 to 0.050 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.0050 | |
| 0 to 0.25 |
| Magnesium (Mg), % | 94 to 97 | |
| 0 |
| Manganese (Mn), % | 0.15 to 0.4 | |
| 0 |
| Nickel (Ni), % | 0 to 0.0050 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.15 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Silicon (Si), % | 0 to 0.1 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 92.5 to 95.5 |
| Vanadium (V), % | 0 | |
| 2.0 to 3.0 |
| Zinc (Zn), % | 0.5 to 1.5 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |