EN 1.4419 Stainless Steel vs. S15500 Stainless Steel
Both EN 1.4419 stainless steel and S15500 stainless steel are iron alloys. They have a moderately high 91% of their average alloy composition in common. There are 32 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is EN 1.4419 stainless steel and the bottom bar is S15500 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 11 to 17 | |
| 6.8 to 16 |
| Fatigue Strength, MPa | 230 to 680 | |
| 350 to 650 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 76 | |
| 75 |
| Shear Strength, MPa | 410 to 950 | |
| 540 to 870 |
| Tensile Strength: Ultimate (UTS), MPa | 660 to 1590 | |
| 890 to 1490 |
| Tensile Strength: Yield (Proof), MPa | 370 to 1240 | |
| 590 to 1310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 390 | |
| 440 |
| Maximum Temperature: Mechanical, °C | 790 | |
| 820 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1430 |
| Melting Onset (Solidus), °C | 1400 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 480 |
| Thermal Conductivity, W/m-K | 30 | |
| 17 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.8 | |
| 2.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.2 | |
| 2.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 8.0 | |
| 13 |
| Density, g/cm3 | 7.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 2.2 | |
| 2.7 |
| Embodied Energy, MJ/kg | 30 | |
| 39 |
| Embodied Water, L/kg | 110 | |
| 130 |
Common Calculations
| PREN (Pitting Resistance) | 16 | |
| 15 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 95 to 170 | |
| 98 to 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 to 3920 | |
| 890 to 4460 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 24 to 57 | |
| 32 to 53 |
| Strength to Weight: Bending, points | 22 to 39 | |
| 26 to 37 |
| Thermal Diffusivity, mm2/s | 8.1 | |
| 4.6 |
| Thermal Shock Resistance, points | 23 to 55 | |
| 30 to 50 |
Alloy Composition
| Carbon (C), % | 0.36 to 0.42 | |
| 0 to 0.070 |
| Chromium (Cr), % | 13 to 14.5 | |
| 14 to 15.5 |
| Copper (Cu), % | 0 | |
| 2.5 to 4.5 |
| Iron (Fe), % | 82 to 86 | |
| 71.9 to 79.9 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0.6 to 1.0 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 3.5 to 5.5 |
| Niobium (Nb), % | 0 | |
| 0.15 to 0.45 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.030 |