EN 1.4606 Stainless Steel vs. Grade 29 Titanium
EN 1.4606 stainless steel belongs to the iron alloys classification, while grade 29 titanium belongs to the titanium alloys. There are 30 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 EN 1.4606 stainless steel and the bottom bar is grade 29 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 110 |
| Elongation at Break, % | 23 to 39 | |
| 6.8 to 11 |
| Fatigue Strength, MPa | 240 to 420 | |
| 460 to 510 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Shear Modulus, GPa | 75 | |
| 40 |
| Shear Strength, MPa | 410 to 640 | |
| 550 to 560 |
| Tensile Strength: Ultimate (UTS), MPa | 600 to 1020 | |
| 930 to 940 |
| Tensile Strength: Yield (Proof), MPa | 280 to 630 | |
| 850 to 870 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 910 | |
| 340 |
| Melting Completion (Liquidus), °C | 1430 | |
| 1610 |
| Melting Onset (Solidus), °C | 1380 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 560 |
| Thermal Conductivity, W/m-K | 14 | |
| 7.3 |
| Thermal Expansion, µm/m-K | 11 | |
| 9.3 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.9 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.2 | |
| 2.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 26 | |
| 36 |
| Density, g/cm3 | 7.9 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 6.0 | |
| 39 |
| Embodied Energy, MJ/kg | 87 | |
| 640 |
| Embodied Water, L/kg | 170 | |
| 410 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 190 to 200 | |
| 62 to 100 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 200 to 1010 | |
| 3420 to 3540 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 35 |
| Strength to Weight: Axial, points | 21 to 36 | |
| 58 to 59 |
| Strength to Weight: Bending, points | 20 to 28 | |
| 47 to 48 |
| Thermal Diffusivity, mm2/s | 3.7 | |
| 2.9 |
| Thermal Shock Resistance, points | 21 to 35 | |
| 68 to 69 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.35 | |
| 5.5 to 6.5 |
| Boron (B), % | 0.0010 to 0.010 | |
| 0 |
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.080 |
| Chromium (Cr), % | 13 to 16 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 49.2 to 59 | |
| 0 to 0.25 |
| Manganese (Mn), % | 1.0 to 2.0 | |
| 0 |
| Molybdenum (Mo), % | 1.0 to 1.5 | |
| 0 |
| Nickel (Ni), % | 24 to 27 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.13 |
| Phosphorus (P), % | 0 to 0.025 | |
| 0 |
| Ruthenium (Ru), % | 0 | |
| 0.080 to 0.14 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 1.9 to 2.3 | |
| 88 to 90.9 |
| Vanadium (V), % | 0.1 to 0.5 | |
| 3.5 to 4.5 |
| Residuals, % | 0 | |
| 0 to 0.4 |