EN 1.4020 Stainless Steel vs. EN 1.4567 Stainless Steel
Both EN 1.4020 stainless steel and EN 1.4567 stainless steel are iron alloys. They have 88% 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 EN 1.4020 stainless steel and the bottom bar is EN 1.4567 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 190 to 340 | |
| 190 to 240 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 13 to 34 | |
| 22 to 51 |
| Fatigue Strength, MPa | 340 to 540 | |
| 190 to 260 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 76 |
| Shear Strength, MPa | 510 to 680 | |
| 390 to 490 |
| Tensile Strength: Ultimate (UTS), MPa | 770 to 1130 | |
| 550 to 780 |
| Tensile Strength: Yield (Proof), MPa | 430 to 950 | |
| 200 to 390 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 290 |
| Maximum Temperature: Corrosion, °C | 410 | |
| 420 |
| Maximum Temperature: Mechanical, °C | 890 | |
| 930 |
| Melting Completion (Liquidus), °C | 1390 | |
| 1410 |
| Melting Onset (Solidus), °C | 1350 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 480 |
| Thermal Expansion, µm/m-K | 17 | |
| 17 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 16 |
| Density, g/cm3 | 7.6 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 2.5 | |
| 3.1 |
| Embodied Energy, MJ/kg | 37 | |
| 43 |
| Embodied Water, L/kg | 150 | |
| 150 |
Common Calculations
| PREN (Pitting Resistance) | 23 | |
| 19 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 220 | |
| 150 to 220 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 2290 | |
| 100 to 400 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 28 to 41 | |
| 19 to 27 |
| Strength to Weight: Bending, points | 25 to 32 | |
| 19 to 24 |
| Thermal Shock Resistance, points | 16 to 23 | |
| 12 to 17 |
Alloy Composition
| Carbon (C), % | 0 to 0.15 | |
| 0 to 0.040 |
| Chromium (Cr), % | 16.5 to 19 | |
| 17 to 19 |
| Copper (Cu), % | 0 | |
| 3.0 to 4.0 |
| Iron (Fe), % | 62.8 to 71.8 | |
| 63.3 to 71.5 |
| Manganese (Mn), % | 11 to 14 | |
| 0 to 2.0 |
| Nickel (Ni), % | 0.5 to 2.5 | |
| 8.5 to 10.5 |
| Nitrogen (N), % | 0.2 to 0.45 | |
| 0 to 0.1 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 to 0.045 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.015 |