6110A Aluminum vs. Grade 28 Titanium
6110A aluminum belongs to the aluminum alloys classification, while grade 28 titanium belongs to the titanium alloys. There are 30 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 6110A aluminum and the bottom bar is grade 28 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 110 |
| Elongation at Break, % | 11 to 18 | |
| 11 to 17 |
| Fatigue Strength, MPa | 140 to 210 | |
| 330 to 480 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 26 | |
| 40 |
| Shear Strength, MPa | 220 to 280 | |
| 420 to 590 |
| Tensile Strength: Ultimate (UTS), MPa | 360 to 470 | |
| 690 to 980 |
| Tensile Strength: Yield (Proof), MPa | 250 to 430 | |
| 540 to 810 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 330 |
| Melting Completion (Liquidus), °C | 650 | |
| 1640 |
| Melting Onset (Solidus), °C | 600 | |
| 1590 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 550 |
| Thermal Conductivity, W/m-K | 160 | |
| 8.3 |
| Thermal Expansion, µm/m-K | 23 | |
| 9.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 42 | |
| 1.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
| 2.7 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 36 |
| Density, g/cm3 | 2.8 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 8.4 | |
| 37 |
| Embodied Energy, MJ/kg | 150 | |
| 600 |
| Embodied Water, L/kg | 1170 | |
| 370 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 47 to 58 | |
| 87 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 450 to 1300 | |
| 1370 to 3100 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 35 |
| Strength to Weight: Axial, points | 36 to 47 | |
| 43 to 61 |
| Strength to Weight: Bending, points | 41 to 48 | |
| 39 to 49 |
| Thermal Diffusivity, mm2/s | 65 | |
| 3.4 |
| Thermal Shock Resistance, points | 16 to 21 | |
| 47 to 66 |
Alloy Composition
| Aluminum (Al), % | 94.8 to 98 | |
| 2.5 to 3.5 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0.050 to 0.25 | |
| 0 |
| Copper (Cu), % | 0.3 to 0.8 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.5 | |
| 0 to 0.25 |
| Magnesium (Mg), % | 0.7 to 1.1 | |
| 0 |
| Manganese (Mn), % | 0.3 to 0.9 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.15 |
| Ruthenium (Ru), % | 0 | |
| 0.080 to 0.14 |
| Silicon (Si), % | 0.7 to 1.1 | |
| 0 |
| Titanium (Ti), % | 0 to 0.2 | |
| 92.4 to 95.4 |
| Vanadium (V), % | 0 | |
| 2.0 to 3.0 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Zirconium (Zr), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |