SAE-AISI 8620 Steel vs. S20910 Stainless Steel
Both SAE-AISI 8620 steel and S20910 stainless steel are iron alloys. They have 59% 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 SAE-AISI 8620 steel and the bottom bar is S20910 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 150 to 210 | |
| 230 to 290 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 200 |
| Elongation at Break, % | 13 to 31 | |
| 14 to 39 |
| Fatigue Strength, MPa | 270 to 360 | |
| 310 to 460 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 73 | |
| 79 |
| Shear Strength, MPa | 340 to 420 | |
| 500 to 570 |
| Tensile Strength: Ultimate (UTS), MPa | 520 to 690 | |
| 780 to 940 |
| Tensile Strength: Yield (Proof), MPa | 360 to 570 | |
| 430 to 810 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 300 |
| Maximum Temperature: Mechanical, °C | 410 | |
| 1080 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1420 |
| Melting Onset (Solidus), °C | 1420 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Conductivity, W/m-K | 39 | |
| 13 |
| Thermal Expansion, µm/m-K | 13 | |
| 16 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.6 | |
| 22 |
| Density, g/cm3 | 7.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 1.5 | |
| 4.8 |
| Embodied Energy, MJ/kg | 20 | |
| 68 |
| Embodied Water, L/kg | 50 | |
| 180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 86 to 150 | |
| 120 to 260 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 340 to 880 | |
| 460 to 1640 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 18 to 24 | |
| 28 to 33 |
| Strength to Weight: Bending, points | 18 to 22 | |
| 24 to 27 |
| Thermal Diffusivity, mm2/s | 10 | |
| 3.6 |
| Thermal Shock Resistance, points | 15 to 20 | |
| 17 to 21 |
Alloy Composition
| Carbon (C), % | 0.18 to 0.23 | |
| 0 to 0.060 |
| Chromium (Cr), % | 0.4 to 0.6 | |
| 20.5 to 23.5 |
| Iron (Fe), % | 96.9 to 98 | |
| 52.1 to 62.1 |
| Manganese (Mn), % | 0.7 to 0.9 | |
| 4.0 to 6.0 |
| Molybdenum (Mo), % | 0.15 to 0.25 | |
| 1.5 to 3.0 |
| Nickel (Ni), % | 0.4 to 0.7 | |
| 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 0.035 | |
| 0 to 0.040 |
| Silicon (Si), % | 0.15 to 0.35 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.040 | |
| 0 to 0.030 |
| Vanadium (V), % | 0 | |
| 0.1 to 0.3 |