Hot Rolled S20910 Stainless Steel vs. Hot Worked Nickel 600
Hot rolled S20910 stainless steel belongs to the iron alloys classification, while hot worked nickel 600 belongs to the nickel alloys. They have a modest 37% of their average alloy composition in common, which, by itself, doesn't mean much. There are 28 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.
For each property being compared, the top bar is hot rolled S20910 stainless steel and the bottom bar is hot worked nickel 600.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 23 | |
| 28 |
| Fatigue Strength, MPa | 310 | |
| 280 |
| Poisson's Ratio | 0.28 | |
| 0.29 |
| Shear Modulus, GPa | 79 | |
| 75 |
| Shear Strength, MPa | 500 | |
| 430 |
| Tensile Strength: Ultimate (UTS), MPa | 790 | |
| 660 |
| Tensile Strength: Yield (Proof), MPa | 460 | |
| 270 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 310 |
| Maximum Temperature: Mechanical, °C | 1080 | |
| 1100 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1410 |
| Melting Onset (Solidus), °C | 1380 | |
| 1350 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 460 |
| Thermal Conductivity, W/m-K | 13 | |
| 14 |
| Thermal Expansion, µm/m-K | 16 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 22 | |
| 55 |
| Density, g/cm3 | 7.8 | |
| 8.5 |
| Embodied Carbon, kg CO2/kg material | 4.8 | |
| 9.0 |
| Embodied Energy, MJ/kg | 68 | |
| 130 |
| Embodied Water, L/kg | 180 | |
| 250 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 | |
| 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 540 | |
| 190 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 23 |
| Strength to Weight: Axial, points | 28 | |
| 22 |
| Strength to Weight: Bending, points | 24 | |
| 20 |
| Thermal Diffusivity, mm2/s | 3.6 | |
| 3.6 |
| Thermal Shock Resistance, points | 18 | |
| 19 |
Alloy Composition
| Carbon (C), % | 0 to 0.060 | |
| 0 to 0.15 |
| Chromium (Cr), % | 20.5 to 23.5 | |
| 14 to 17 |
| Copper (Cu), % | 0 | |
| 0 to 0.5 |
| Iron (Fe), % | 52.1 to 62.1 | |
| 6.0 to 10 |
| Manganese (Mn), % | 4.0 to 6.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 1.5 to 3.0 | |
| 0 |
| Nickel (Ni), % | 11.5 to 13.5 | |
| 72 to 80 |
| Niobium (Nb), % | 0.1 to 0.3 | |
| 0 |
| Nitrogen (N), % | 0.2 to 0.4 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 0 to 0.75 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.015 |
| Vanadium (V), % | 0.1 to 0.3 | |
| 0 |