Grade 5 Titanium vs. Grade 19 Titanium
Both grade 5 titanium and grade 19 titanium are titanium alloys. They have 82% of their average alloy composition in common. There are 29 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is grade 5 titanium and the bottom bar is grade 19 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 120 |
| Elongation at Break, % | 8.6 to 11 | |
| 5.6 to 17 |
| Fatigue Strength, MPa | 530 to 630 | |
| 550 to 620 |
| Poisson's Ratio | 0.32 | |
| 0.32 |
| Reduction in Area, % | 21 to 25 | |
| 22 |
| Shear Modulus, GPa | 40 | |
| 47 |
| Shear Strength, MPa | 600 to 710 | |
| 550 to 750 |
| Tensile Strength: Ultimate (UTS), MPa | 1000 to 1190 | |
| 890 to 1300 |
| Tensile Strength: Yield (Proof), MPa | 910 to 1110 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 330 | |
| 370 |
| Melting Completion (Liquidus), °C | 1610 | |
| 1660 |
| Melting Onset (Solidus), °C | 1650 | |
| 1600 |
| Specific Heat Capacity, J/kg-K | 560 | |
| 520 |
| Thermal Conductivity, W/m-K | 6.8 | |
| 6.2 |
| Thermal Expansion, µm/m-K | 8.9 | |
| 9.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 36 | |
| 45 |
| Density, g/cm3 | 4.4 | |
| 5.0 |
| Embodied Carbon, kg CO2/kg material | 38 | |
| 47 |
| Embodied Energy, MJ/kg | 610 | |
| 760 |
| Embodied Water, L/kg | 200 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 100 to 110 | |
| 70 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 3980 to 5880 | |
| 3040 to 5530 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 35 | |
| 33 |
| Strength to Weight: Axial, points | 62 to 75 | |
| 49 to 72 |
| Strength to Weight: Bending, points | 50 to 56 | |
| 41 to 53 |
| Thermal Diffusivity, mm2/s | 2.7 | |
| 2.4 |
| Thermal Shock Resistance, points | 76 to 91 | |
| 57 to 83 |
Alloy Composition
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| Aluminum (Al), % | 5.5 to 6.8 | |
| 3.0 to 4.0 |
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.050 |
| Chromium (Cr), % | 0 | |
| 5.5 to 6.5 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 to 0.020 |
| Iron (Fe), % | 0 to 0.4 | |
| 0 to 0.3 |
| Molybdenum (Mo), % | 0 | |
| 3.5 to 4.5 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 to 0.2 | |
| 0 to 0.12 |
| Titanium (Ti), % | 87.4 to 91 | |
| 71.1 to 77 |
| Vanadium (V), % | 3.5 to 4.5 | |
| 7.5 to 8.5 |
| Yttrium (Y), % | 0 to 0.0050 | |
| 0 |
| Zirconium (Zr), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 to 0.4 | |
| 0 to 0.4 |