Grade 5 Titanium vs. EN 1.4606 Stainless Steel
Grade 5 titanium belongs to the titanium alloys classification, while EN 1.4606 stainless steel belongs to the iron alloys. There are 30 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 5 titanium and the bottom bar is EN 1.4606 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 190 |
| Elongation at Break, % | 8.6 to 11 | |
| 23 to 39 |
| Fatigue Strength, MPa | 530 to 630 | |
| 240 to 420 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Shear Modulus, GPa | 40 | |
| 75 |
| Shear Strength, MPa | 600 to 710 | |
| 410 to 640 |
| Tensile Strength: Ultimate (UTS), MPa | 1000 to 1190 | |
| 600 to 1020 |
| Tensile Strength: Yield (Proof), MPa | 910 to 1110 | |
| 280 to 630 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 300 |
| Maximum Temperature: Mechanical, °C | 330 | |
| 910 |
| Melting Completion (Liquidus), °C | 1610 | |
| 1430 |
| Melting Onset (Solidus), °C | 1650 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 560 | |
| 470 |
| Thermal Conductivity, W/m-K | 6.8 | |
| 14 |
| Thermal Expansion, µm/m-K | 8.9 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
| 1.9 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
| 2.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 36 | |
| 26 |
| Density, g/cm3 | 4.4 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 38 | |
| 6.0 |
| Embodied Energy, MJ/kg | 610 | |
| 87 |
| Embodied Water, L/kg | 200 | |
| 170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 100 to 110 | |
| 190 to 200 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 3980 to 5880 | |
| 200 to 1010 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 35 | |
| 24 |
| Strength to Weight: Axial, points | 62 to 75 | |
| 21 to 36 |
| Strength to Weight: Bending, points | 50 to 56 | |
| 20 to 28 |
| Thermal Diffusivity, mm2/s | 2.7 | |
| 3.7 |
| Thermal Shock Resistance, points | 76 to 91 | |
| 21 to 35 |
Alloy Composition
| Aluminum (Al), % | 5.5 to 6.8 | |
| 0 to 0.35 |
| Boron (B), % | 0 | |
| 0.0010 to 0.010 |
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0 | |
| 13 to 16 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 49.2 to 59 |
| Manganese (Mn), % | 0 | |
| 1.0 to 2.0 |
| Molybdenum (Mo), % | 0 | |
| 1.0 to 1.5 |
| Nickel (Ni), % | 0 | |
| 24 to 27 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 |
| Oxygen (O), % | 0 to 0.2 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Titanium (Ti), % | 87.4 to 91 | |
| 1.9 to 2.3 |
| Vanadium (V), % | 3.5 to 4.5 | |
| 0.1 to 0.5 |
| Yttrium (Y), % | 0 to 0.0050 | |
| 0 |
| Residuals, % | 0 to 0.4 | |
| 0 |