S46910 Stainless Steel vs. AISI 201LN Stainless Steel
Both S46910 stainless steel and AISI 201LN stainless steel are iron alloys. They have 88% of their average alloy composition in common. 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 S46910 stainless steel and the bottom bar is AISI 201LN stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 270 to 630 | |
| 210 to 320 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 2.2 to 11 | |
| 25 to 51 |
| Fatigue Strength, MPa | 250 to 1020 | |
| 340 to 540 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 76 | |
| 77 |
| Shear Strength, MPa | 410 to 1410 | |
| 530 to 680 |
| Tensile Strength: Ultimate (UTS), MPa | 680 to 2470 | |
| 740 to 1060 |
| Tensile Strength: Yield (Proof), MPa | 450 to 2290 | |
| 350 to 770 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 540 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 810 | |
| 880 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1410 |
| Melting Onset (Solidus), °C | 1420 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Expansion, µm/m-K | 11 | |
| 17 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 18 | |
| 12 |
| Density, g/cm3 | 7.9 | |
| 7.7 |
| Embodied Carbon, kg CO2/kg material | 4.1 | |
| 2.6 |
| Embodied Energy, MJ/kg | 55 | |
| 38 |
| Embodied Water, L/kg | 140 | |
| 140 |
Common Calculations
| PREN (Pitting Resistance) | 25 | |
| 20 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 48 to 130 | |
| 230 to 310 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 510 to 4780 | |
| 310 to 1520 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 24 to 86 | |
| 27 to 38 |
| Strength to Weight: Bending, points | 22 to 51 | |
| 24 to 30 |
| Thermal Shock Resistance, points | 23 to 84 | |
| 16 to 23 |
Alloy Composition
| Aluminum (Al), % | 0.15 to 0.5 | |
| 0 |
| Carbon (C), % | 0 to 0.030 | |
| 0 to 0.030 |
| Chromium (Cr), % | 11 to 13 | |
| 16 to 17.5 |
| Copper (Cu), % | 1.5 to 3.5 | |
| 0 to 1.0 |
| Iron (Fe), % | 65 to 76 | |
| 67.9 to 73.5 |
| Manganese (Mn), % | 0 to 1.0 | |
| 6.4 to 7.5 |
| Molybdenum (Mo), % | 3.0 to 5.0 | |
| 0 |
| Nickel (Ni), % | 8.0 to 10 | |
| 4.0 to 5.0 |
| Nitrogen (N), % | 0 | |
| 0.1 to 0.25 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.045 |
| Silicon (Si), % | 0 to 0.7 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0.5 to 1.2 | |
| 0 |