6110A Aluminum vs. Grade 21 Titanium
6110A aluminum belongs to the aluminum alloys classification, while grade 21 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.
For each property being compared, the top bar is 6110A aluminum and the bottom bar is grade 21 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 140 |
| Elongation at Break, % | 11 to 18 | |
| 9.0 to 17 |
| Fatigue Strength, MPa | 140 to 210 | |
| 550 to 660 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 26 | |
| 51 |
| Shear Strength, MPa | 220 to 280 | |
| 550 to 790 |
| Tensile Strength: Ultimate (UTS), MPa | 360 to 470 | |
| 890 to 1340 |
| Tensile Strength: Yield (Proof), MPa | 250 to 430 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 310 |
| Melting Completion (Liquidus), °C | 650 | |
| 1740 |
| Melting Onset (Solidus), °C | 600 | |
| 1690 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 500 |
| Thermal Conductivity, W/m-K | 160 | |
| 7.5 |
| Thermal Expansion, µm/m-K | 23 | |
| 7.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 60 |
| Density, g/cm3 | 2.8 | |
| 5.4 |
| Embodied Carbon, kg CO2/kg material | 8.4 | |
| 32 |
| Embodied Energy, MJ/kg | 150 | |
| 490 |
| Embodied Water, L/kg | 1170 | |
| 180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 47 to 58 | |
| 110 to 180 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 450 to 1300 | |
| 2760 to 5010 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 50 | |
| 32 |
| Strength to Weight: Axial, points | 36 to 47 | |
| 46 to 69 |
| Strength to Weight: Bending, points | 41 to 48 | |
| 38 to 50 |
| Thermal Diffusivity, mm2/s | 65 | |
| 2.8 |
| Thermal Shock Resistance, points | 16 to 21 | |
| 66 to 100 |
Alloy Composition
| Aluminum (Al), % | 94.8 to 98 | |
| 2.5 to 3.5 |
| Carbon (C), % | 0 | |
| 0 to 0.050 |
| 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 0.4 |
| Magnesium (Mg), % | 0.7 to 1.1 | |
| 0 |
| Manganese (Mn), % | 0.3 to 0.9 | |
| 0 |
| Molybdenum (Mo), % | 0 | |
| 14 to 16 |
| Niobium (Nb), % | 0 | |
| 2.2 to 3.2 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.17 |
| Silicon (Si), % | 0.7 to 1.1 | |
| 0.15 to 0.25 |
| Titanium (Ti), % | 0 to 0.2 | |
| 76 to 81.2 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Zirconium (Zr), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |