S13800 Stainless Steel vs. EN 1.4542 Stainless Steel
Both S13800 stainless steel and EN 1.4542 stainless steel are iron alloys. They have a moderately high 92% of their average alloy composition in common. There are 32 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 S13800 stainless steel and the bottom bar is EN 1.4542 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 11 to 18 | |
| 5.7 to 20 |
| Fatigue Strength, MPa | 410 to 870 | |
| 370 to 640 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 76 |
| Shear Strength, MPa | 610 to 1030 | |
| 550 to 860 |
| Tensile Strength: Ultimate (UTS), MPa | 980 to 1730 | |
| 880 to 1470 |
| Tensile Strength: Yield (Proof), MPa | 660 to 1580 | |
| 580 to 1300 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 390 | |
| 440 |
| Maximum Temperature: Mechanical, °C | 810 | |
| 860 |
| Melting Completion (Liquidus), °C | 1450 | |
| 1430 |
| Melting Onset (Solidus), °C | 1410 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 470 |
| Thermal Conductivity, W/m-K | 16 | |
| 16 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
| 2.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
| 2.8 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 15 | |
| 13 |
| Density, g/cm3 | 7.9 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 3.4 | |
| 2.7 |
| Embodied Energy, MJ/kg | 46 | |
| 39 |
| Embodied Water, L/kg | 140 | |
| 130 |
Common Calculations
| PREN (Pitting Resistance) | 21 | |
| 17 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 190 | |
| 62 to 160 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1090 to 5490 | |
| 880 to 4360 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 35 to 61 | |
| 31 to 52 |
| Strength to Weight: Bending, points | 28 to 41 | |
| 26 to 37 |
| Thermal Diffusivity, mm2/s | 4.3 | |
| 4.3 |
| Thermal Shock Resistance, points | 33 to 58 | |
| 29 to 49 |
Alloy Composition
| Aluminum (Al), % | 0.9 to 1.4 | |
| 0 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.070 |
| Chromium (Cr), % | 12.3 to 13.2 | |
| 15 to 17 |
| Copper (Cu), % | 0 | |
| 3.0 to 5.0 |
| Iron (Fe), % | 73.6 to 77.3 | |
| 69.6 to 79 |
| Manganese (Mn), % | 0 to 0.2 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 2.0 to 3.0 | |
| 0 to 0.6 |
| Nickel (Ni), % | 7.5 to 8.5 | |
| 3.0 to 5.0 |
| Niobium (Nb), % | 0 | |
| 0 to 0.45 |
| Nitrogen (N), % | 0 to 0.010 | |
| 0 |
| Phosphorus (P), % | 0 to 0.010 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.1 | |
| 0 to 0.7 |
| Sulfur (S), % | 0 to 0.0080 | |
| 0 to 0.015 |