EN 1.4912 Stainless Steel vs. EN 1.4557 Stainless Steel
Both EN 1.4912 stainless steel and EN 1.4557 stainless steel are iron alloys. Both are furnished in the solution annealed (AT) condition. They have 83% of their average alloy composition in common. There are 33 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is EN 1.4912 stainless steel and the bottom bar is EN 1.4557 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 180 | |
| 160 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 40 | |
| 40 |
| Fatigue Strength, MPa | 200 | |
| 260 |
| Impact Strength: V-Notched Charpy, J | 90 | |
| 56 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 80 |
| Tensile Strength: Ultimate (UTS), MPa | 610 | |
| 560 |
| Tensile Strength: Yield (Proof), MPa | 230 | |
| 300 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 300 |
| Maximum Temperature: Corrosion, °C | 520 | |
| 420 |
| Maximum Temperature: Mechanical, °C | 940 | |
| 1090 |
| Melting Completion (Liquidus), °C | 1430 | |
| 1460 |
| Melting Onset (Solidus), °C | 1390 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 460 |
| Thermal Conductivity, W/m-K | 16 | |
| 15 |
| Thermal Expansion, µm/m-K | 16 | |
| 17 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.4 | |
| 2.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 2.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 20 | |
| 29 |
| Density, g/cm3 | 7.8 | |
| 8.0 |
| Embodied Carbon, kg CO2/kg material | 3.8 | |
| 5.6 |
| Embodied Energy, MJ/kg | 55 | |
| 76 |
| Embodied Water, L/kg | 140 | |
| 190 |
Common Calculations
| PREN (Pitting Resistance) | 18 | |
| 45 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 190 | |
| 190 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 130 | |
| 210 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 24 |
| Strength to Weight: Axial, points | 22 | |
| 19 |
| Strength to Weight: Bending, points | 20 | |
| 19 |
| Thermal Diffusivity, mm2/s | 4.2 | |
| 4.0 |
| Thermal Shock Resistance, points | 14 | |
| 12 |
Alloy Composition
| Carbon (C), % | 0.040 to 0.1 | |
| 0 to 0.020 |
| Chromium (Cr), % | 17 to 19 | |
| 19.5 to 20.5 |
| Copper (Cu), % | 0 | |
| 0.5 to 1.0 |
| Iron (Fe), % | 64.6 to 73.6 | |
| 49.5 to 56.3 |
| Manganese (Mn), % | 0 to 2.0 | |
| 0 to 1.2 |
| Molybdenum (Mo), % | 0 | |
| 6.0 to 7.0 |
| Nickel (Ni), % | 9.0 to 12 | |
| 17.5 to 19.5 |
| Niobium (Nb), % | 0.4 to 1.2 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0.18 to 0.24 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.010 |