EN 1.4568 Stainless Steel vs. Grade 19 Titanium
EN 1.4568 stainless steel belongs to the iron alloys classification, while grade 19 titanium belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is EN 1.4568 stainless steel and the bottom bar is grade 19 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 120 |
| Elongation at Break, % | 2.3 to 21 | |
| 5.6 to 17 |
| Fatigue Strength, MPa | 220 to 670 | |
| 550 to 620 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 76 | |
| 47 |
| Shear Strength, MPa | 520 to 930 | |
| 550 to 750 |
| Tensile Strength: Ultimate (UTS), MPa | 830 to 1620 | |
| 890 to 1300 |
| Tensile Strength: Yield (Proof), MPa | 330 to 1490 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 890 | |
| 370 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1660 |
| Melting Onset (Solidus), °C | 1380 | |
| 1600 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 520 |
| Thermal Conductivity, W/m-K | 16 | |
| 6.2 |
| Thermal Expansion, µm/m-K | 13 | |
| 9.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 13 | |
| 45 |
| Density, g/cm3 | 7.7 | |
| 5.0 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 47 |
| Embodied Energy, MJ/kg | 40 | |
| 760 |
| Embodied Water, L/kg | 140 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 36 to 140 | |
| 70 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 290 to 5710 | |
| 3040 to 5530 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 33 |
| Strength to Weight: Axial, points | 30 to 58 | |
| 49 to 72 |
| Strength to Weight: Bending, points | 25 to 40 | |
| 41 to 53 |
| Thermal Diffusivity, mm2/s | 4.3 | |
| 2.4 |
| Thermal Shock Resistance, points | 23 to 46 | |
| 57 to 83 |
Alloy Composition
| Aluminum (Al), % | 0.7 to 1.5 | |
| 3.0 to 4.0 |
| Carbon (C), % | 0 to 0.090 | |
| 0 to 0.050 |
| Chromium (Cr), % | 16 to 18 | |
| 5.5 to 6.5 |
| Hydrogen (H), % | 0 | |
| 0 to 0.020 |
| Iron (Fe), % | 70.9 to 76.8 | |
| 0 to 0.3 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 |
| Molybdenum (Mo), % | 0 | |
| 3.5 to 4.5 |
| Nickel (Ni), % | 6.5 to 7.8 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.12 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 0 to 0.7 | |
| 0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 71.1 to 77 |
| Vanadium (V), % | 0 | |
| 7.5 to 8.5 |
| Zirconium (Zr), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 | |
| 0 to 0.4 |