242.0 Aluminum vs. Grade 18 Titanium
242.0 aluminum belongs to the aluminum alloys classification, while grade 18 titanium belongs to the titanium 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 242.0 aluminum and the bottom bar is grade 18 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 73 | |
| 110 |
| Elongation at Break, % | 0.5 to 1.5 | |
| 11 to 17 |
| Fatigue Strength, MPa | 55 to 110 | |
| 330 to 480 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 27 | |
| 40 |
| Shear Strength, MPa | 150 to 240 | |
| 420 to 590 |
| Tensile Strength: Ultimate (UTS), MPa | 180 to 290 | |
| 690 to 980 |
| Tensile Strength: Yield (Proof), MPa | 120 to 220 | |
| 540 to 810 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 210 | |
| 330 |
| Melting Completion (Liquidus), °C | 640 | |
| 1640 |
| Melting Onset (Solidus), °C | 530 | |
| 1590 |
| Specific Heat Capacity, J/kg-K | 870 | |
| 550 |
| Thermal Conductivity, W/m-K | 130 to 170 | |
| 8.3 |
| Thermal Expansion, µm/m-K | 22 | |
| 9.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 33 to 44 | |
| 1.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 96 to 130 | |
| 2.7 |
Otherwise Unclassified Properties
| Density, g/cm3 | 3.1 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 41 |
| Embodied Energy, MJ/kg | 150 | |
| 670 |
| Embodied Water, L/kg | 1130 | |
| 270 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 1.3 to 3.4 | |
| 87 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 340 | |
| 1380 to 3110 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 45 | |
| 35 |
| Strength to Weight: Axial, points | 16 to 26 | |
| 43 to 61 |
| Strength to Weight: Bending, points | 23 to 32 | |
| 39 to 49 |
| Thermal Diffusivity, mm2/s | 50 to 62 | |
| 3.4 |
| Thermal Shock Resistance, points | 8.0 to 13 | |
| 47 to 67 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
| Aluminum (Al), % | 88.4 to 93.6 | |
| 2.5 to 3.5 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0 to 0.25 | |
| 0 |
| Copper (Cu), % | 3.5 to 4.5 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 1.0 | |
| 0 to 0.25 |
| Magnesium (Mg), % | 1.2 to 1.8 | |
| 0 |
| Manganese (Mn), % | 0 to 0.35 | |
| 0 |
| Nickel (Ni), % | 1.7 to 2.3 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.15 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Silicon (Si), % | 0 to 0.7 | |
| 0 |
| Titanium (Ti), % | 0 to 0.25 | |
| 92.5 to 95.5 |
| Vanadium (V), % | 0 | |
| 2.0 to 3.0 |
| Zinc (Zn), % | 0 to 0.35 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.4 |