S35500 Stainless Steel vs. S46910 Stainless Steel
Both S35500 stainless steel and S46910 stainless steel are iron alloys. They have a moderately high 91% 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 S35500 stainless steel and the bottom bar is S46910 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 14 | |
| 2.2 to 11 |
| Fatigue Strength, MPa | 690 to 730 | |
| 250 to 1020 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Rockwell C Hardness | 33 to 42 | |
| 29 to 63 |
| Shear Modulus, GPa | 78 | |
| 76 |
| Shear Strength, MPa | 810 to 910 | |
| 410 to 1410 |
| Tensile Strength: Ultimate (UTS), MPa | 1330 to 1490 | |
| 680 to 2470 |
| Tensile Strength: Yield (Proof), MPa | 1200 to 1280 | |
| 450 to 2290 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 440 | |
| 540 |
| Maximum Temperature: Mechanical, °C | 870 | |
| 810 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1460 |
| Melting Onset (Solidus), °C | 1420 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 470 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 16 | |
| 18 |
| Density, g/cm3 | 7.8 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 3.5 | |
| 4.1 |
| Embodied Energy, MJ/kg | 47 | |
| 55 |
| Embodied Water, L/kg | 130 | |
| 140 |
Common Calculations
| PREN (Pitting Resistance) | 27 | |
| 25 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 180 to 190 | |
| 48 to 130 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 3610 to 4100 | |
| 510 to 4780 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 24 |
| Strength to Weight: Axial, points | 47 to 53 | |
| 24 to 86 |
| Strength to Weight: Bending, points | 34 to 37 | |
| 22 to 51 |
| Thermal Shock Resistance, points | 44 to 49 | |
| 23 to 84 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0.15 to 0.5 |
| Carbon (C), % | 0.1 to 0.15 | |
| 0 to 0.030 |
| Chromium (Cr), % | 15 to 16 | |
| 11 to 13 |
| Copper (Cu), % | 0 | |
| 1.5 to 3.5 |
| Iron (Fe), % | 73.2 to 77.7 | |
| 65 to 76 |
| Manganese (Mn), % | 0.5 to 1.3 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 2.5 to 3.2 | |
| 3.0 to 5.0 |
| Nickel (Ni), % | 4.0 to 5.0 | |
| 8.0 to 10 |
| Niobium (Nb), % | 0.1 to 0.5 | |
| 0 |
| Nitrogen (N), % | 0.070 to 0.13 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.7 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 | |
| 0.5 to 1.2 |