2030 Aluminum vs. Grade 23 Titanium
2030 aluminum belongs to the aluminum alloys classification, while grade 23 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 2030 aluminum and the bottom bar is grade 23 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 110 |
| Elongation at Break, % | 5.6 to 8.0 | |
| 6.7 to 11 |
| Fatigue Strength, MPa | 91 to 110 | |
| 470 to 500 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 26 | |
| 40 |
| Shear Strength, MPa | 220 to 250 | |
| 540 to 570 |
| Tensile Strength: Ultimate (UTS), MPa | 370 to 420 | |
| 930 to 940 |
| Tensile Strength: Yield (Proof), MPa | 240 to 270 | |
| 850 to 870 |
Thermal Properties
| Latent Heat of Fusion, J/g | 390 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 340 |
| Melting Completion (Liquidus), °C | 640 | |
| 1610 |
| Melting Onset (Solidus), °C | 510 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 870 | |
| 560 |
| Thermal Conductivity, W/m-K | 130 | |
| 7.1 |
| Thermal Expansion, µm/m-K | 23 | |
| 9.4 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 34 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 99 | |
| 2.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 10 | |
| 36 |
| Density, g/cm3 | 3.1 | |
| 4.4 |
| Embodied Carbon, kg CO2/kg material | 8.0 | |
| 38 |
| Embodied Energy, MJ/kg | 150 | |
| 610 |
| Embodied Water, L/kg | 1140 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 21 to 26 | |
| 61 to 100 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 390 to 530 | |
| 3430 to 3560 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 45 | |
| 35 |
| Strength to Weight: Axial, points | 33 to 38 | |
| 58 to 59 |
| Strength to Weight: Bending, points | 37 to 40 | |
| 48 |
| Thermal Diffusivity, mm2/s | 50 | |
| 2.9 |
| Thermal Shock Resistance, points | 16 to 19 | |
| 67 to 68 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
| Aluminum (Al), % | 88.9 to 95.2 | |
| 5.5 to 6.5 |
| Bismuth (Bi), % | 0 to 0.2 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0 to 0.1 | |
| 0 |
| Copper (Cu), % | 3.3 to 4.5 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.013 |
| Iron (Fe), % | 0 to 0.7 | |
| 0 to 0.25 |
| Lead (Pb), % | 0.8 to 1.5 | |
| 0 |
| Magnesium (Mg), % | 0.5 to 1.3 | |
| 0 |
| Manganese (Mn), % | 0.2 to 1.0 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.13 |
| Silicon (Si), % | 0 to 0.8 | |
| 0 |
| Titanium (Ti), % | 0 to 0.2 | |
| 88.1 to 91 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Zinc (Zn), % | 0 to 0.5 | |
| 0 |
| Residuals, % | 0 to 0.3 | |
| 0 to 0.4 |