Titanium 6-2-4-2 vs. 354.0 Aluminum
Titanium 6-2-4-2 belongs to the titanium alloys classification, while 354.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is titanium 6-2-4-2 and the bottom bar is 354.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 71 |
| Elongation at Break, % | 8.6 | |
| 2.4 to 3.0 |
| Fatigue Strength, MPa | 490 | |
| 92 to 120 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 40 | |
| 27 |
| Tensile Strength: Ultimate (UTS), MPa | 950 | |
| 360 to 380 |
| Tensile Strength: Yield (Proof), MPa | 880 | |
| 280 to 310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 530 |
| Maximum Temperature: Mechanical, °C | 300 | |
| 170 |
| Melting Completion (Liquidus), °C | 1590 | |
| 600 |
| Melting Onset (Solidus), °C | 1540 | |
| 550 |
| Specific Heat Capacity, J/kg-K | 540 | |
| 900 |
| Thermal Conductivity, W/m-K | 6.9 | |
| 130 |
| Thermal Expansion, µm/m-K | 9.5 | |
| 21 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 0.9 | |
| 32 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.8 | |
| 110 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 42 | |
| 9.5 |
| Density, g/cm3 | 4.6 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 32 | |
| 7.8 |
| Embodied Energy, MJ/kg | 520 | |
| 150 |
| Embodied Water, L/kg | 210 | |
| 1070 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 79 | |
| 8.6 to 9.8 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 3640 | |
| 540 to 670 |
| Stiffness to Weight: Axial, points | 13 | |
| 15 |
| Stiffness to Weight: Bending, points | 34 | |
| 52 |
| Strength to Weight: Axial, points | 57 | |
| 37 to 39 |
| Strength to Weight: Bending, points | 46 | |
| 42 to 44 |
| Thermal Diffusivity, mm2/s | 2.8 | |
| 52 |
| Thermal Shock Resistance, points | 67 | |
| 17 to 18 |
Alloy Composition
| Aluminum (Al), % | 5.5 to 6.5 | |
| 87.3 to 89.4 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Copper (Cu), % | 0 | |
| 1.6 to 2.0 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.25 | |
| 0 to 0.2 |
| Magnesium (Mg), % | 0 | |
| 0.4 to 0.6 |
| Manganese (Mn), % | 0 | |
| 0 to 0.1 |
| Molybdenum (Mo), % | 1.8 to 2.2 | |
| 0 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 |
| Oxygen (O), % | 0 to 0.15 | |
| 0 |
| Silicon (Si), % | 0.060 to 0.12 | |
| 8.6 to 9.4 |
| Tin (Sn), % | 1.8 to 2.2 | |
| 0 |
| Titanium (Ti), % | 83.7 to 87.2 | |
| 0 to 0.2 |
| Zinc (Zn), % | 0 | |
| 0 to 0.1 |
| Zirconium (Zr), % | 3.6 to 4.4 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.15 |