Grade 28 Titanium vs. Grade 6 Titanium
Both grade 28 titanium and grade 6 titanium are titanium alloys. They have a very high 95% of their average alloy composition in common.
For each property being compared, the top bar is grade 28 titanium and the bottom bar is grade 6 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 100 | 
| Elongation at Break, % | 11 to 17 | |
| 11 | 
| Fatigue Strength, MPa | 330 to 480 | |
| 290 | 
| Poisson's Ratio | 0.32 | |
| 0.32 | 
| Reduction in Area, % | 22 | |
| 27 | 
| Shear Modulus, GPa | 40 | |
| 39 | 
| Shear Strength, MPa | 420 to 590 | |
| 530 | 
| Tensile Strength: Ultimate (UTS), MPa | 690 to 980 | |
| 890 | 
| Tensile Strength: Yield (Proof), MPa | 540 to 810 | |
| 840 | 
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 410 | 
| Maximum Temperature: Mechanical, °C | 330 | |
| 310 | 
| Melting Completion (Liquidus), °C | 1640 | |
| 1580 | 
| Melting Onset (Solidus), °C | 1590 | |
| 1530 | 
| Specific Heat Capacity, J/kg-K | 550 | |
| 550 | 
| Thermal Conductivity, W/m-K | 8.3 | |
| 7.8 | 
| Thermal Expansion, µm/m-K | 9.9 | |
| 9.4 | 
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
| 1.2 | 
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 2.5 | 
Otherwise Unclassified Properties
| Base Metal Price, % relative | 36 | |
| 36 | 
| Density, g/cm3 | 4.5 | |
| 4.5 | 
| Embodied Carbon, kg CO2/kg material | 37 | |
| 30 | 
| Embodied Energy, MJ/kg | 600 | |
| 480 | 
| Embodied Water, L/kg | 370 | |
| 190 | 
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 87 to 110 | |
| 92 | 
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1370 to 3100 | |
| 3390 | 
| Stiffness to Weight: Axial, points | 13 | |
| 13 | 
| Stiffness to Weight: Bending, points | 35 | |
| 35 | 
| Strength to Weight: Axial, points | 43 to 61 | |
| 55 | 
| Strength to Weight: Bending, points | 39 to 49 | |
| 46 | 
| Thermal Diffusivity, mm2/s | 3.4 | |
| 3.2 | 
| Thermal Shock Resistance, points | 47 to 66 | |
| 65 | 
Alloy Composition
| Aluminum (Al), % | 2.5 to 3.5 | |
| 4.0 to 6.0 | 
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.080 | 
| Hydrogen (H), % | 0 to 0.015 | |
| 0 to 0.015 | 
| Iron (Fe), % | 0 to 0.25 | |
| 0 to 0.5 | 
| Nitrogen (N), % | 0 to 0.030 | |
| 0 to 0.030 | 
| Oxygen (O), % | 0 to 0.15 | |
| 0 to 0.2 | 
| Ruthenium (Ru), % | 0.080 to 0.14 | |
| 0 | 
| Tin (Sn), % | 0 | |
| 2.0 to 3.0 | 
| Titanium (Ti), % | 92.4 to 95.4 | |
| 89.8 to 94 | 
| Vanadium (V), % | 2.0 to 3.0 | |
| 0 | 
| Residuals, % | 0 | |
| 0 to 0.4 |