Grade 20 Titanium vs. 358.0 Aluminum
Grade 20 titanium belongs to the titanium alloys classification, while 358.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is grade 20 titanium and the bottom bar is 358.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 120 | |
| 71 |
| Elongation at Break, % | 5.7 to 17 | |
| 3.5 to 6.0 |
| Fatigue Strength, MPa | 550 to 630 | |
| 100 to 110 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 47 | |
| 27 |
| Shear Strength, MPa | 560 to 740 | |
| 300 to 320 |
| Tensile Strength: Ultimate (UTS), MPa | 900 to 1270 | |
| 350 to 370 |
| Tensile Strength: Yield (Proof), MPa | 850 to 1190 | |
| 290 to 320 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 520 |
| Maximum Temperature: Mechanical, °C | 370 | |
| 170 |
| Melting Completion (Liquidus), °C | 1660 | |
| 600 |
| Melting Onset (Solidus), °C | 1600 | |
| 560 |
| Specific Heat Capacity, J/kg-K | 520 | |
| 900 |
| Thermal Expansion, µm/m-K | 9.6 | |
| 21 |
Otherwise Unclassified Properties
| Density, g/cm3 | 5.0 | |
| 2.6 |
| Embodied Carbon, kg CO2/kg material | 52 | |
| 8.7 |
| Embodied Energy, MJ/kg | 860 | |
| 160 |
| Embodied Water, L/kg | 350 | |
| 1090 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 71 to 150 | |
| 12 to 20 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2940 to 5760 | |
| 590 to 710 |
| Stiffness to Weight: Axial, points | 14 | |
| 15 |
| Stiffness to Weight: Bending, points | 33 | |
| 53 |
| Strength to Weight: Axial, points | 50 to 70 | |
| 37 to 39 |
| Strength to Weight: Bending, points | 41 to 52 | |
| 42 to 44 |
| Thermal Shock Resistance, points | 55 to 77 | |
| 16 to 17 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
| Aluminum (Al), % | 3.0 to 4.0 | |
| 89.1 to 91.8 |
| Beryllium (Be), % | 0 | |
| 0.1 to 0.3 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 5.5 to 6.5 | |
| 0 to 0.2 |
| Copper (Cu), % | 0 | |
| 0 to 0.2 |
| Hydrogen (H), % | 0 to 0.020 | |
| 0 |
| Iron (Fe), % | 0 to 0.3 | |
| 0 to 0.3 |
| Magnesium (Mg), % | 0 | |
| 0.4 to 0.6 |
| Manganese (Mn), % | 0 | |
| 0 to 0.2 |
| Molybdenum (Mo), % | 3.5 to 4.5 | |
| 0 |
| Nitrogen (N), % | 0 to 0.030 | |
| 0 |
| Oxygen (O), % | 0 to 0.12 | |
| 0 |
| Palladium (Pd), % | 0.040 to 0.080 | |
| 0 |
| Silicon (Si), % | 0 | |
| 7.6 to 8.6 |
| Titanium (Ti), % | 71 to 77 | |
| 0.1 to 0.2 |
| Vanadium (V), % | 7.5 to 8.5 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Zirconium (Zr), % | 3.5 to 4.5 | |
| 0 |
| Residuals, % | 0 to 0.4 | |
| 0 to 0.15 |