S46910 Stainless Steel vs. S45500 Stainless Steel
Both S46910 stainless steel and S45500 stainless steel are iron alloys. They have a moderately high 94% of their average alloy composition in common. There are 29 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is S46910 stainless steel and the bottom bar is S45500 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 270 to 630 | |
| 280 to 500 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 2.2 to 11 | |
| 3.4 to 11 |
| Fatigue Strength, MPa | 250 to 1020 | |
| 570 to 890 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Rockwell C Hardness | 29 to 63 | |
| 32 to 54 |
| Shear Modulus, GPa | 76 | |
| 75 |
| Shear Strength, MPa | 410 to 1410 | |
| 790 to 1090 |
| Tensile Strength: Ultimate (UTS), MPa | 680 to 2470 | |
| 1370 to 1850 |
| Tensile Strength: Yield (Proof), MPa | 450 to 2290 | |
| 1240 to 1700 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 270 |
| Maximum Temperature: Corrosion, °C | 540 | |
| 620 |
| Maximum Temperature: Mechanical, °C | 810 | |
| 760 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1440 |
| Melting Onset (Solidus), °C | 1420 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 470 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 18 | |
| 17 |
| Density, g/cm3 | 7.9 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 4.1 | |
| 3.8 |
| Embodied Energy, MJ/kg | 55 | |
| 57 |
| Embodied Water, L/kg | 140 | |
| 120 |
Common Calculations
| PREN (Pitting Resistance) | 25 | |
| 13 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 48 to 130 | |
| 45 to 190 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 24 |
| Strength to Weight: Axial, points | 24 to 86 | |
| 48 to 65 |
| Strength to Weight: Bending, points | 22 to 51 | |
| 35 to 42 |
| Thermal Shock Resistance, points | 23 to 84 | |
| 48 to 64 |
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 | |
| 11 to 12.5 |
| Copper (Cu), % | 1.5 to 3.5 | |
| 1.5 to 2.5 |
| Iron (Fe), % | 65 to 76 | |
| 71.5 to 79.2 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 3.0 to 5.0 | |
| 0 to 0.5 |
| Nickel (Ni), % | 8.0 to 10 | |
| 7.5 to 9.5 |
| Niobium (Nb), % | 0 | |
| 0 to 0.5 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.7 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.030 |
| Tantalum (Ta), % | 0 | |
| 0 to 0.5 |
| Titanium (Ti), % | 0.5 to 1.2 | |
| 0.8 to 1.4 |