S46910 Stainless Steel vs. S15500 Stainless Steel
Both S46910 stainless steel and S15500 stainless steel are iron alloys. They have a moderately high 90% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is S46910 stainless steel and the bottom bar is S15500 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 270 to 630 | |
| 290 to 430 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 2.2 to 11 | |
| 6.8 to 16 |
| Fatigue Strength, MPa | 250 to 1020 | |
| 350 to 650 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Rockwell C Hardness | 29 to 63 | |
| 27 to 46 |
| Shear Modulus, GPa | 76 | |
| 75 |
| Shear Strength, MPa | 410 to 1410 | |
| 540 to 870 |
| Tensile Strength: Ultimate (UTS), MPa | 680 to 2470 | |
| 890 to 1490 |
| Tensile Strength: Yield (Proof), MPa | 450 to 2290 | |
| 590 to 1310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 540 | |
| 440 |
| Maximum Temperature: Mechanical, °C | 810 | |
| 820 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1430 |
| Melting Onset (Solidus), °C | 1420 | |
| 1380 |
| 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 | |
| 2.7 |
| Embodied Energy, MJ/kg | 55 | |
| 39 |
| Embodied Water, L/kg | 140 | |
| 130 |
Common Calculations
| PREN (Pitting Resistance) | 25 | |
| 15 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 48 to 130 | |
| 98 to 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 510 to 4780 | |
| 890 to 4460 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 24 to 86 | |
| 32 to 53 |
| Strength to Weight: Bending, points | 22 to 51 | |
| 26 to 37 |
| Thermal Shock Resistance, points | 23 to 84 | |
| 30 to 50 |
Alloy Composition
| Aluminum (Al), % | 0.15 to 0.5 | |
| 0 |
| Carbon (C), % | 0 to 0.030 | |
| 0 to 0.070 |
| Chromium (Cr), % | 11 to 13 | |
| 14 to 15.5 |
| Copper (Cu), % | 1.5 to 3.5 | |
| 2.5 to 4.5 |
| Iron (Fe), % | 65 to 76 | |
| 71.9 to 79.9 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 3.0 to 5.0 | |
| 0 |
| Nickel (Ni), % | 8.0 to 10 | |
| 3.5 to 5.5 |
| Niobium (Nb), % | 0 | |
| 0.15 to 0.45 |
| 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 |