Cold Rolled EN 1.4062 vs. Strain Hardened S20910 Stainless Steel
Both cold rolled EN 1.4062 and strain hardened S20910 stainless steel are iron alloys. Both are furnished in the cold worked (strain hardened) condition. They have 83% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is cold rolled EN 1.4062 and the bottom bar is strain hardened S20910 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 23 | |
| 14 |
| Fatigue Strength, MPa | 410 | |
| 460 |
| Poisson's Ratio | 0.27 | |
| 0.28 |
| Shear Modulus, GPa | 79 | |
| 79 |
| Shear Strength, MPa | 510 | |
| 570 |
| Tensile Strength: Ultimate (UTS), MPa | 800 | |
| 940 |
| Tensile Strength: Yield (Proof), MPa | 600 | |
| 810 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 300 |
| Maximum Temperature: Corrosion, °C | 440 | |
| 460 |
| Maximum Temperature: Mechanical, °C | 1030 | |
| 1080 |
| Melting Completion (Liquidus), °C | 1430 | |
| 1420 |
| Melting Onset (Solidus), °C | 1380 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 480 |
| Thermal Conductivity, W/m-K | 15 | |
| 13 |
| Thermal Expansion, µm/m-K | 13 | |
| 16 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 22 |
| Density, g/cm3 | 7.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 2.6 | |
| 4.8 |
| Embodied Energy, MJ/kg | 37 | |
| 68 |
| Embodied Water, L/kg | 150 | |
| 180 |
Common Calculations
| PREN (Pitting Resistance) | 27 | |
| 34 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 170 | |
| 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 910 | |
| 1640 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 29 | |
| 33 |
| Strength to Weight: Bending, points | 25 | |
| 27 |
| Thermal Diffusivity, mm2/s | 4.0 | |
| 3.6 |
| Thermal Shock Resistance, points | 22 | |
| 21 |
Alloy Composition
| Carbon (C), % | 0 to 0.030 | |
| 0 to 0.060 |
| Chromium (Cr), % | 21.5 to 24 | |
| 20.5 to 23.5 |
| Iron (Fe), % | 69.3 to 77.3 | |
| 52.1 to 62.1 |
| Manganese (Mn), % | 0 to 2.0 | |
| 4.0 to 6.0 |
| Molybdenum (Mo), % | 0 to 0.45 | |
| 1.5 to 3.0 |
| Nickel (Ni), % | 1.0 to 2.9 | |
| 11.5 to 13.5 |
| Niobium (Nb), % | 0 | |
| 0.1 to 0.3 |
| Nitrogen (N), % | 0.16 to 0.28 | |
| 0.2 to 0.4 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 to 0.030 |
| Vanadium (V), % | 0 | |
| 0.1 to 0.3 |