6262A Aluminum vs. Grade 20 Titanium
6262A aluminum belongs to the aluminum alloys classification, while grade 20 titanium belongs to the titanium 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 6262A aluminum and the bottom bar is grade 20 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 68 | |
| 120 |
| Elongation at Break, % | 4.5 to 11 | |
| 5.7 to 17 |
| Fatigue Strength, MPa | 94 to 110 | |
| 550 to 630 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 26 | |
| 47 |
| Shear Strength, MPa | 190 to 240 | |
| 560 to 740 |
| Tensile Strength: Ultimate (UTS), MPa | 310 to 410 | |
| 900 to 1270 |
| Tensile Strength: Yield (Proof), MPa | 270 to 370 | |
| 850 to 1190 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 370 |
| Melting Completion (Liquidus), °C | 640 | |
| 1660 |
| Melting Onset (Solidus), °C | 580 | |
| 1600 |
| Specific Heat Capacity, J/kg-K | 890 | |
| 520 |
| Thermal Expansion, µm/m-K | 23 | |
| 9.6 |
Otherwise Unclassified Properties
| Density, g/cm3 | 2.8 | |
| 5.0 |
| Embodied Carbon, kg CO2/kg material | 8.4 | |
| 52 |
| Embodied Energy, MJ/kg | 150 | |
| 860 |
| Embodied Water, L/kg | 1190 | |
| 350 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 17 to 34 | |
| 71 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 540 to 1000 | |
| 2940 to 5760 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 49 | |
| 33 |
| Strength to Weight: Axial, points | 31 to 41 | |
| 50 to 70 |
| Strength to Weight: Bending, points | 36 to 44 | |
| 41 to 52 |
| Thermal Shock Resistance, points | 14 to 18 | |
| 55 to 77 |
Alloy Composition
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| Aluminum (Al), % | 94.2 to 97.8 | |
| 3.0 to 4.0 |
| Bismuth (Bi), % | 0.4 to 0.9 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.050 |
| Chromium (Cr), % | 0.040 to 0.14 | |
| 5.5 to 6.5 |
| Copper (Cu), % | 0.15 to 0.4 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.020 |
| Iron (Fe), % | 0 to 0.7 | |
| 0 to 0.3 |
| Magnesium (Mg), % | 0.8 to 1.2 | |
| 0 |
| Manganese (Mn), % | 0 to 0.15 | |
| 0 |
| Molybdenum (Mo), % | 0 | |
| 3.5 to 4.5 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.12 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Silicon (Si), % | 0.4 to 0.8 | |
| 0 |
| Tin (Sn), % | 0.4 to 1.0 | |
| 0 |
| Titanium (Ti), % | 0 to 0.1 | |
| 71 to 77 |
| Vanadium (V), % | 0 | |
| 7.5 to 8.5 |
| Zinc (Zn), % | 0 to 0.25 | |
| 0 |
| Zirconium (Zr), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.4 |