Hot Finished AISI 310 vs. Hot Rolled S20910 Stainless Steel
Both hot finished AISI 310 and hot rolled S20910 stainless steel are iron alloys. Both are furnished in the hot worked condition. They have 89% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is hot finished AISI 310 and the bottom bar is hot rolled S20910 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 180 | |
| 240 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 45 | |
| 23 |
| Fatigue Strength, MPa | 240 | |
| 310 |
| Poisson's Ratio | 0.27 | |
| 0.28 |
| Shear Modulus, GPa | 78 | |
| 79 |
| Shear Strength, MPa | 420 | |
| 500 |
| Tensile Strength: Ultimate (UTS), MPa | 600 | |
| 790 |
| Tensile Strength: Yield (Proof), MPa | 260 | |
| 460 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 300 |
| Maximum Temperature: Corrosion, °C | 440 | |
| 460 |
| Maximum Temperature: Mechanical, °C | 1040 | |
| 1080 |
| Melting Completion (Liquidus), °C | 1450 | |
| 1420 |
| Melting Onset (Solidus), °C | 1400 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 480 |
| Thermal Conductivity, W/m-K | 15 | |
| 13 |
| Thermal Expansion, µm/m-K | 15 | |
| 16 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 25 | |
| 22 |
| Density, g/cm3 | 7.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 4.3 | |
| 4.8 |
| Embodied Energy, MJ/kg | 61 | |
| 68 |
| Embodied Water, L/kg | 190 | |
| 180 |
Common Calculations
| PREN (Pitting Resistance) | 25 | |
| 34 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 220 | |
| 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 | |
| 540 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 21 | |
| 28 |
| Strength to Weight: Bending, points | 20 | |
| 24 |
| Thermal Diffusivity, mm2/s | 3.9 | |
| 3.6 |
| Thermal Shock Resistance, points | 14 | |
| 18 |
Alloy Composition
| Carbon (C), % | 0 to 0.25 | |
| 0 to 0.060 |
| Chromium (Cr), % | 24 to 26 | |
| 20.5 to 23.5 |
| Iron (Fe), % | 48.2 to 57 | |
| 52.1 to 62.1 |
| Manganese (Mn), % | 0 to 2.0 | |
| 4.0 to 6.0 |
| Molybdenum (Mo), % | 0 | |
| 1.5 to 3.0 |
| Nickel (Ni), % | 19 to 22 | |
| 11.5 to 13.5 |
| Niobium (Nb), % | 0 | |
| 0.1 to 0.3 |
| Nitrogen (N), % | 0 | |
| 0.2 to 0.4 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 1.5 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.030 |
| Vanadium (V), % | 0 | |
| 0.1 to 0.3 |