Annealed Titanium 4-4-2 vs. Annealed Titanium 6-6-2
Both annealed titanium 4-4-2 and annealed titanium 6-6-2 are titanium alloys. Both are furnished in the annealed condition. They have a very high 96% of their average alloy composition in common.
For each property being compared, the top bar is annealed titanium 4-4-2 and the bottom bar is annealed titanium 6-6-2.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 120 |
| Elongation at Break, % | 10 | |
| 9.0 |
| Fatigue Strength, MPa | 590 | |
| 590 |
| Poisson's Ratio | 0.32 | |
| 0.32 |
| Reduction in Area, % | 20 | |
| 23 |
| Shear Modulus, GPa | 42 | |
| 44 |
| Shear Strength, MPa | 690 | |
| 670 |
| Tensile Strength: Ultimate (UTS), MPa | 1150 | |
| 1140 |
| Tensile Strength: Yield (Proof), MPa | 1030 | |
| 1040 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 310 | |
| 310 |
| Melting Completion (Liquidus), °C | 1610 | |
| 1610 |
| Melting Onset (Solidus), °C | 1560 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 540 | |
| 540 |
| Thermal Conductivity, W/m-K | 6.7 | |
| 5.5 |
| Thermal Expansion, µm/m-K | 8.6 | |
| 9.4 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.1 | |
| 1.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.1 | |
| 2.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 39 | |
| 40 |
| Density, g/cm3 | 4.7 | |
| 4.8 |
| Embodied Carbon, kg CO2/kg material | 30 | |
| 29 |
| Embodied Energy, MJ/kg | 480 | |
| 470 |
| Embodied Water, L/kg | 180 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 | |
| 99 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 4700 | |
| 4710 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 34 | |
| 34 |
| Strength to Weight: Axial, points | 68 | |
| 66 |
| Strength to Weight: Bending, points | 52 | |
| 50 |
| Thermal Diffusivity, mm2/s | 2.6 | |
| 2.1 |
| Thermal Shock Resistance, points | 86 | |
| 75 |
Alloy Composition
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| Aluminum (Al), % | 3.0 to 5.0 | |
| 5.0 to 6.0 |
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.050 |
| Copper (Cu), % | 0 | |
| 0.35 to 1.0 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.2 | |
| 0.35 to 1.0 |
| Molybdenum (Mo), % | 3.0 to 5.0 | |
| 5.0 to 6.0 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 to 0.040 |
| Oxygen (O), % | 0 to 0.25 | |
| 0 to 0.2 |
| Silicon (Si), % | 0.3 to 0.7 | |
| 0 |
| Tin (Sn), % | 1.5 to 2.5 | |
| 1.5 to 2.5 |
| Titanium (Ti), % | 85.8 to 92.2 | |
| 82.8 to 87.8 |
| Residuals, % | 0 to 0.4 | |
| 0 to 0.4 |