Grade 18 Titanium vs. 242.0 Aluminum
Grade 18 titanium belongs to the titanium alloys classification, while 242.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is grade 18 titanium and the bottom bar is 242.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 73 |
| Elongation at Break, % | 11 to 17 | |
| 0.5 to 1.5 |
| Fatigue Strength, MPa | 330 to 480 | |
| 55 to 110 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 40 | |
| 27 |
| Shear Strength, MPa | 420 to 590 | |
| 150 to 240 |
| Tensile Strength: Ultimate (UTS), MPa | 690 to 980 | |
| 180 to 290 |
| Tensile Strength: Yield (Proof), MPa | 540 to 810 | |
| 120 to 220 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 330 | |
| 210 |
| Melting Completion (Liquidus), °C | 1640 | |
| 640 |
| Melting Onset (Solidus), °C | 1590 | |
| 530 |
| Specific Heat Capacity, J/kg-K | 550 | |
| 870 |
| Thermal Conductivity, W/m-K | 8.3 | |
| 130 to 170 |
| Thermal Expansion, µm/m-K | 9.9 | |
| 22 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
| 33 to 44 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 96 to 130 |
Otherwise Unclassified Properties
| Density, g/cm3 | 4.5 | |
| 3.1 |
| Embodied Carbon, kg CO2/kg material | 41 | |
| 8.3 |
| Embodied Energy, MJ/kg | 670 | |
| 150 |
| Embodied Water, L/kg | 270 | |
| 1130 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 87 to 110 | |
| 1.3 to 3.4 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1380 to 3110 | |
| 110 to 340 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 35 | |
| 45 |
| Strength to Weight: Axial, points | 43 to 61 | |
| 16 to 26 |
| Strength to Weight: Bending, points | 39 to 49 | |
| 23 to 32 |
| Thermal Diffusivity, mm2/s | 3.4 | |
| 50 to 62 |
| Thermal Shock Resistance, points | 47 to 67 | |
| 8.0 to 13 |
Alloy Composition
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| Aluminum (Al), % | 2.5 to 3.5 | |
| 88.4 to 93.6 |
| Carbon (C), % | 0 to 0.080 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.25 |
| Copper (Cu), % | 0 | |
| 3.5 to 4.5 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.25 | |
| 0 to 1.0 |
| Magnesium (Mg), % | 0 | |
| 1.2 to 1.8 |
| Manganese (Mn), % | 0 | |
| 0 to 0.35 |
| Nickel (Ni), % | 0 | |
| 1.7 to 2.3 |
| Nitrogen (N), % | 0 to 0.030 | |
| 0 |
| Oxygen (O), % | 0 to 0.15 | |
| 0 |
| Palladium (Pd), % | 0.040 to 0.080 | |
| 0 |
| Silicon (Si), % | 0 | |
| 0 to 0.7 |
| Titanium (Ti), % | 92.5 to 95.5 | |
| 0 to 0.25 |
| Vanadium (V), % | 2.0 to 3.0 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.35 |
| Residuals, % | 0 to 0.4 | |
| 0 to 0.15 |