S20910 Stainless Steel vs. EN 1.7386 Steel
Both S20910 stainless steel and EN 1.7386 steel are iron alloys. They have 68% of their average alloy composition in common. There are 30 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 S20910 stainless steel and the bottom bar is EN 1.7386 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 230 to 290 | |
| 170 to 200 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 14 to 39 | |
| 18 to 21 |
| Fatigue Strength, MPa | 310 to 460 | |
| 170 to 290 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 79 | |
| 75 |
| Shear Strength, MPa | 500 to 570 | |
| 340 to 410 |
| Tensile Strength: Ultimate (UTS), MPa | 780 to 940 | |
| 550 to 670 |
| Tensile Strength: Yield (Proof), MPa | 430 to 810 | |
| 240 to 440 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 270 |
| Maximum Temperature: Mechanical, °C | 1080 | |
| 600 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1450 |
| Melting Onset (Solidus), °C | 1380 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 480 |
| Thermal Conductivity, W/m-K | 13 | |
| 26 |
| Thermal Expansion, µm/m-K | 16 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 22 | |
| 6.5 |
| Density, g/cm3 | 7.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 4.8 | |
| 2.0 |
| Embodied Energy, MJ/kg | 68 | |
| 28 |
| Embodied Water, L/kg | 180 | |
| 88 |
Common Calculations
| PREN (Pitting Resistance) | 34 | |
| 12 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 120 to 260 | |
| 92 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 1640 | |
| 150 to 490 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 28 to 33 | |
| 20 to 24 |
| Strength to Weight: Bending, points | 24 to 27 | |
| 19 to 22 |
| Thermal Diffusivity, mm2/s | 3.6 | |
| 6.9 |
| Thermal Shock Resistance, points | 17 to 21 | |
| 15 to 18 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.040 |
| Carbon (C), % | 0 to 0.060 | |
| 0.080 to 0.15 |
| Chromium (Cr), % | 20.5 to 23.5 | |
| 8.0 to 10 |
| Copper (Cu), % | 0 | |
| 0 to 0.3 |
| Iron (Fe), % | 52.1 to 62.1 | |
| 86.8 to 90.5 |
| Manganese (Mn), % | 4.0 to 6.0 | |
| 0.3 to 0.6 |
| Molybdenum (Mo), % | 1.5 to 3.0 | |
| 0.9 to 1.1 |
| Nickel (Ni), % | 11.5 to 13.5 | |
| 0 |
| Niobium (Nb), % | 0.1 to 0.3 | |
| 0 |
| Nitrogen (N), % | 0.2 to 0.4 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 to 0.75 | |
| 0.25 to 1.0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.010 |
| Vanadium (V), % | 0.1 to 0.3 | |
| 0 |