S46910 Stainless Steel vs. S45000 Stainless Steel
Both S46910 stainless steel and S45000 stainless steel are iron alloys. They have a moderately high 92% 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 S46910 stainless steel and the bottom bar is S45000 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 270 to 630 | |
| 280 to 410 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 2.2 to 11 | |
| 6.8 to 14 |
| Fatigue Strength, MPa | 250 to 1020 | |
| 330 to 650 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Rockwell C Hardness | 29 to 63 | |
| 28 to 44 |
| Shear Modulus, GPa | 76 | |
| 76 |
| Shear Strength, MPa | 410 to 1410 | |
| 590 to 830 |
| Tensile Strength: Ultimate (UTS), MPa | 680 to 2470 | |
| 980 to 1410 |
| Tensile Strength: Yield (Proof), MPa | 450 to 2290 | |
| 580 to 1310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 540 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 810 | |
| 840 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1440 |
| Melting Onset (Solidus), °C | 1420 | |
| 1390 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 18 | |
| 13 |
| Density, g/cm3 | 7.9 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 4.1 | |
| 2.8 |
| Embodied Energy, MJ/kg | 55 | |
| 39 |
| Embodied Water, L/kg | 140 | |
| 130 |
Common Calculations
| PREN (Pitting Resistance) | 25 | |
| 17 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 48 to 130 | |
| 94 to 160 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 510 to 4780 | |
| 850 to 4400 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 24 to 86 | |
| 35 to 50 |
| Strength to Weight: Bending, points | 22 to 51 | |
| 28 to 36 |
| Thermal Shock Resistance, points | 23 to 84 | |
| 33 to 47 |
Alloy Composition
| Aluminum (Al), % | 0.15 to 0.5 | |
| 0 |
| Carbon (C), % | 0 to 0.030 | |
| 0 to 0.050 |
| Chromium (Cr), % | 11 to 13 | |
| 14 to 16 |
| Copper (Cu), % | 1.5 to 3.5 | |
| 1.3 to 1.8 |
| Iron (Fe), % | 65 to 76 | |
| 72.1 to 79.3 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 3.0 to 5.0 | |
| 0.5 to 1.0 |
| Nickel (Ni), % | 8.0 to 10 | |
| 5.0 to 7.0 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.7 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0.5 to 1.2 | |
| 0 |