Titanium 6-6-2 vs. EN 1.5525 Steel
Titanium 6-6-2 belongs to the titanium alloys classification, while EN 1.5525 steel belongs to the iron 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 titanium 6-6-2 and the bottom bar is EN 1.5525 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 120 | |
| 190 |
| Elongation at Break, % | 6.7 to 9.0 | |
| 11 to 21 |
| Fatigue Strength, MPa | 590 to 670 | |
| 210 to 310 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Reduction in Area, % | 17 to 23 | |
| 62 to 73 |
| Shear Modulus, GPa | 44 | |
| 73 |
| Shear Strength, MPa | 670 to 800 | |
| 310 to 350 |
| Tensile Strength: Ultimate (UTS), MPa | 1140 to 1370 | |
| 440 to 1440 |
| Tensile Strength: Yield (Proof), MPa | 1040 to 1230 | |
| 300 to 490 |
Thermal Properties
| Latent Heat of Fusion, J/g | 400 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 310 | |
| 400 |
| Melting Completion (Liquidus), °C | 1610 | |
| 1460 |
| Melting Onset (Solidus), °C | 1560 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 540 | |
| 470 |
| Thermal Conductivity, W/m-K | 5.5 | |
| 50 |
| Thermal Expansion, µm/m-K | 9.4 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.1 | |
| 7.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.1 | |
| 8.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 40 | |
| 1.9 |
| Density, g/cm3 | 4.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 29 | |
| 1.4 |
| Embodied Energy, MJ/kg | 470 | |
| 19 |
| Embodied Water, L/kg | 200 | |
| 48 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 89 to 99 | |
| 44 to 240 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 34 | |
| 24 |
| Strength to Weight: Axial, points | 66 to 79 | |
| 16 to 51 |
| Strength to Weight: Bending, points | 50 to 57 | |
| 16 to 36 |
| Thermal Diffusivity, mm2/s | 2.1 | |
| 13 |
| Thermal Shock Resistance, points | 75 to 90 | |
| 13 to 42 |
Alloy Composition
| Aluminum (Al), % | 5.0 to 6.0 | |
| 0 |
| Boron (B), % | 0 | |
| 0.00080 to 0.0050 |
| Carbon (C), % | 0 to 0.050 | |
| 0.18 to 0.23 |
| Chromium (Cr), % | 0 | |
| 0 to 0.3 |
| Copper (Cu), % | 0.35 to 1.0 | |
| 0 to 0.25 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0.35 to 1.0 | |
| 97.7 to 98.9 |
| Manganese (Mn), % | 0 | |
| 0.9 to 1.2 |
| Molybdenum (Mo), % | 5.0 to 6.0 | |
| 0 |
| Nitrogen (N), % | 0 to 0.040 | |
| 0 |
| Oxygen (O), % | 0 to 0.2 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 | |
| 0 to 0.025 |
| Tin (Sn), % | 1.5 to 2.5 | |
| 0 |
| Titanium (Ti), % | 82.8 to 87.8 | |
| 0 |
| Residuals, % | 0 to 0.4 | |
| 0 |