S20910 Stainless Steel vs. EN 1.5414 Steel
Both S20910 stainless steel and EN 1.5414 steel are iron alloys. They have 59% of their average alloy composition in common. There are 29 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is S20910 stainless steel and the bottom bar is EN 1.5414 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 230 to 290 | |
| 170 to 180 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 14 to 39 | |
| 22 |
| Fatigue Strength, MPa | 310 to 460 | |
| 250 to 270 |
| Poisson's Ratio | 0.28 | |
| 0.29 |
| Shear Modulus, GPa | 79 | |
| 73 |
| Shear Strength, MPa | 500 to 570 | |
| 350 to 370 |
| Tensile Strength: Ultimate (UTS), MPa | 780 to 940 | |
| 550 to 580 |
| Tensile Strength: Yield (Proof), MPa | 430 to 810 | |
| 350 to 380 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 1080 | |
| 410 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1470 |
| Melting Onset (Solidus), °C | 1380 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 470 |
| Thermal Conductivity, W/m-K | 13 | |
| 44 |
| Thermal Expansion, µm/m-K | 16 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 22 | |
| 2.6 |
| Density, g/cm3 | 7.8 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 4.8 | |
| 1.6 |
| Embodied Energy, MJ/kg | 68 | |
| 21 |
| Embodied Water, L/kg | 180 | |
| 50 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 120 to 260 | |
| 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 1640 | |
| 320 to 370 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 24 |
| Strength to Weight: Axial, points | 28 to 33 | |
| 19 to 20 |
| Strength to Weight: Bending, points | 24 to 27 | |
| 19 to 20 |
| Thermal Diffusivity, mm2/s | 3.6 | |
| 12 |
| Thermal Shock Resistance, points | 17 to 21 | |
| 16 to 17 |
Alloy Composition
| Carbon (C), % | 0 to 0.060 | |
| 0 to 0.2 |
| Chromium (Cr), % | 20.5 to 23.5 | |
| 0 to 0.3 |
| Copper (Cu), % | 0 | |
| 0 to 0.3 |
| Iron (Fe), % | 52.1 to 62.1 | |
| 96.4 to 98.7 |
| Manganese (Mn), % | 4.0 to 6.0 | |
| 0.9 to 1.5 |
| Molybdenum (Mo), % | 1.5 to 3.0 | |
| 0.45 to 0.6 |
| Nickel (Ni), % | 11.5 to 13.5 | |
| 0 to 0.3 |
| Niobium (Nb), % | 0.1 to 0.3 | |
| 0 |
| Nitrogen (N), % | 0.2 to 0.4 | |
| 0 to 0.012 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.015 |
| Silicon (Si), % | 0 to 0.75 | |
| 0 to 0.4 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.0050 |
| Vanadium (V), % | 0.1 to 0.3 | |
| 0 |