7022 Aluminum vs. Grade 5 Titanium
7022 aluminum belongs to the aluminum alloys classification, while grade 5 titanium belongs to the titanium alloys. There are 30 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 7022 aluminum and the bottom bar is grade 5 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 110 |
| Elongation at Break, % | 6.3 to 8.0 | |
| 8.6 to 11 |
| Fatigue Strength, MPa | 140 to 170 | |
| 530 to 630 |
| Poisson's Ratio | 0.32 | |
| 0.32 |
| Shear Modulus, GPa | 26 | |
| 40 |
| Shear Strength, MPa | 290 to 320 | |
| 600 to 710 |
| Tensile Strength: Ultimate (UTS), MPa | 490 to 540 | |
| 1000 to 1190 |
| Tensile Strength: Yield (Proof), MPa | 390 to 460 | |
| 910 to 1110 |
Thermal Properties
| Latent Heat of Fusion, J/g | 380 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 200 | |
| 330 |
| Melting Completion (Liquidus), °C | 640 | |
| 1610 |
| Melting Onset (Solidus), °C | 480 | |
| 1650 |
| Specific Heat Capacity, J/kg-K | 870 | |
| 560 |
| Thermal Conductivity, W/m-K | 140 | |
| 6.8 |
| Thermal Expansion, µm/m-K | 24 | |
| 8.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 21 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 65 | |
| 2.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 36 |
| Density, g/cm3 | 2.9 | |
| 4.4 |
| Embodied Carbon, kg CO2/kg material | 8.5 | |
| 38 |
| Embodied Energy, MJ/kg | 150 | |
| 610 |
| Embodied Water, L/kg | 1130 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 29 to 40 | |
| 100 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1100 to 1500 | |
| 3980 to 5880 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 47 | |
| 35 |
| Strength to Weight: Axial, points | 47 to 51 | |
| 62 to 75 |
| Strength to Weight: Bending, points | 47 to 50 | |
| 50 to 56 |
| Thermal Diffusivity, mm2/s | 54 | |
| 2.7 |
| Thermal Shock Resistance, points | 21 to 23 | |
| 76 to 91 |
Alloy Composition
| Aluminum (Al), % | 87.9 to 92.4 | |
| 5.5 to 6.8 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0.1 to 0.3 | |
| 0 |
| Copper (Cu), % | 0.5 to 1.0 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.5 | |
| 0 to 0.4 |
| Magnesium (Mg), % | 2.6 to 3.7 | |
| 0 |
| Manganese (Mn), % | 0.1 to 0.4 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 |
| Titanium (Ti), % | 0 to 0.2 | |
| 87.4 to 91 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Yttrium (Y), % | 0 | |
| 0 to 0.0050 |
| Zinc (Zn), % | 4.3 to 5.2 | |
| 0 |
| Zirconium (Zr), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |