Grade 21 Titanium vs. 5059 Aluminum
Grade 21 titanium belongs to the titanium alloys classification, while 5059 aluminum belongs to the aluminum alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is grade 21 titanium and the bottom bar is 5059 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 140 | |
| 69 |
| Elongation at Break, % | 9.0 to 17 | |
| 11 to 25 |
| Fatigue Strength, MPa | 550 to 660 | |
| 170 to 240 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 51 | |
| 26 |
| Shear Strength, MPa | 550 to 790 | |
| 220 to 250 |
| Tensile Strength: Ultimate (UTS), MPa | 890 to 1340 | |
| 350 to 410 |
| Tensile Strength: Yield (Proof), MPa | 870 to 1170 | |
| 170 to 300 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 310 | |
| 210 |
| Melting Completion (Liquidus), °C | 1740 | |
| 650 |
| Melting Onset (Solidus), °C | 1690 | |
| 510 |
| Specific Heat Capacity, J/kg-K | 500 | |
| 900 |
| Thermal Conductivity, W/m-K | 7.5 | |
| 110 |
| Thermal Expansion, µm/m-K | 7.1 | |
| 24 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 9.5 |
| Density, g/cm3 | 5.4 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 32 | |
| 9.1 |
| Embodied Energy, MJ/kg | 490 | |
| 160 |
| Embodied Water, L/kg | 180 | |
| 1160 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 to 180 | |
| 42 to 75 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2760 to 5010 | |
| 220 to 650 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 32 | |
| 50 |
| Strength to Weight: Axial, points | 46 to 69 | |
| 36 to 42 |
| Strength to Weight: Bending, points | 38 to 50 | |
| 41 to 45 |
| Thermal Diffusivity, mm2/s | 2.8 | |
| 44 |
| Thermal Shock Resistance, points | 66 to 100 | |
| 16 to 18 |
Alloy Composition
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| Aluminum (Al), % | 2.5 to 3.5 | |
| 89.9 to 94 |
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.25 |
| Copper (Cu), % | 0 | |
| 0 to 0.25 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 5.0 to 6.0 |
| Manganese (Mn), % | 0 | |
| 0.6 to 1.2 |
| Molybdenum (Mo), % | 14 to 16 | |
| 0 |
| Niobium (Nb), % | 2.2 to 3.2 | |
| 0 |
| Nitrogen (N), % | 0 to 0.030 | |
| 0 |
| Oxygen (O), % | 0 to 0.17 | |
| 0 |
| Silicon (Si), % | 0.15 to 0.25 | |
| 0 to 0.45 |
| Titanium (Ti), % | 76 to 81.2 | |
| 0 to 0.2 |
| Zinc (Zn), % | 0 | |
| 0.4 to 0.9 |
| Zirconium (Zr), % | 0 | |
| 0.050 to 0.25 |
| Residuals, % | 0 to 0.4 | |
| 0 to 0.15 |