EN 1.4923 Stainless Steel vs. Grade 21 Titanium
EN 1.4923 stainless steel belongs to the iron alloys classification, while grade 21 titanium belongs to the titanium alloys. There are 29 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 1.4923 stainless steel and the bottom bar is grade 21 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 140 |
| Elongation at Break, % | 12 to 21 | |
| 9.0 to 17 |
| Fatigue Strength, MPa | 300 to 440 | |
| 550 to 660 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Reduction in Area, % | 40 to 46 | |
| 22 |
| Shear Modulus, GPa | 76 | |
| 51 |
| Shear Strength, MPa | 540 to 590 | |
| 550 to 790 |
| Tensile Strength: Ultimate (UTS), MPa | 870 to 980 | |
| 890 to 1340 |
| Tensile Strength: Yield (Proof), MPa | 470 to 780 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 740 | |
| 310 |
| Melting Completion (Liquidus), °C | 1450 | |
| 1740 |
| Melting Onset (Solidus), °C | 1410 | |
| 1690 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 500 |
| Thermal Conductivity, W/m-K | 24 | |
| 7.5 |
| Thermal Expansion, µm/m-K | 11 | |
| 7.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 8.0 | |
| 60 |
| Density, g/cm3 | 7.8 | |
| 5.4 |
| Embodied Carbon, kg CO2/kg material | 2.9 | |
| 32 |
| Embodied Energy, MJ/kg | 41 | |
| 490 |
| Embodied Water, L/kg | 100 | |
| 180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 to 150 | |
| 110 to 180 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 570 to 1580 | |
| 2760 to 5010 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 32 |
| Strength to Weight: Axial, points | 31 to 35 | |
| 46 to 69 |
| Strength to Weight: Bending, points | 26 to 28 | |
| 38 to 50 |
| Thermal Diffusivity, mm2/s | 6.5 | |
| 2.8 |
| Thermal Shock Resistance, points | 30 to 34 | |
| 66 to 100 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 2.5 to 3.5 |
| Carbon (C), % | 0.18 to 0.24 | |
| 0 to 0.050 |
| Chromium (Cr), % | 11 to 12.5 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 83.5 to 87.1 | |
| 0 to 0.4 |
| Manganese (Mn), % | 0.4 to 0.9 | |
| 0 |
| Molybdenum (Mo), % | 0.8 to 1.2 | |
| 14 to 16 |
| Nickel (Ni), % | 0.3 to 0.8 | |
| 0 |
| Niobium (Nb), % | 0 | |
| 2.2 to 3.2 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.17 |
| Phosphorus (P), % | 0 to 0.025 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0.15 to 0.25 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 76 to 81.2 |
| Vanadium (V), % | 0.25 to 0.35 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |