EN 1.4415 Stainless Steel vs. Nickel 693
EN 1.4415 stainless steel belongs to the iron alloys classification, while nickel 693 belongs to the nickel alloys. They have a modest 23% of their average alloy composition in common, which, by itself, doesn't mean much. There are 28 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 1.4415 stainless steel and the bottom bar is nickel 693.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 17 to 20 | |
| 34 |
| Fatigue Strength, MPa | 470 to 510 | |
| 230 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 76 |
| Shear Strength, MPa | 520 to 570 | |
| 440 |
| Tensile Strength: Ultimate (UTS), MPa | 830 to 930 | |
| 660 |
| Tensile Strength: Yield (Proof), MPa | 730 to 840 | |
| 310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 330 |
| Maximum Temperature: Mechanical, °C | 790 | |
| 1010 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1350 |
| Melting Onset (Solidus), °C | 1420 | |
| 1310 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Conductivity, W/m-K | 19 | |
| 9.1 |
| Thermal Expansion, µm/m-K | 9.9 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 13 | |
| 60 |
| Density, g/cm3 | 7.9 | |
| 8.1 |
| Embodied Carbon, kg CO2/kg material | 3.6 | |
| 9.9 |
| Embodied Energy, MJ/kg | 51 | |
| 140 |
| Embodied Water, L/kg | 120 | |
| 320 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 160 | |
| 190 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1350 to 1790 | |
| 250 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 24 |
| Strength to Weight: Axial, points | 29 to 33 | |
| 23 |
| Strength to Weight: Bending, points | 25 to 27 | |
| 21 |
| Thermal Diffusivity, mm2/s | 5.1 | |
| 2.3 |
| Thermal Shock Resistance, points | 30 to 34 | |
| 19 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 2.5 to 4.0 |
| Carbon (C), % | 0 to 0.030 | |
| 0 to 0.15 |
| Chromium (Cr), % | 11.5 to 13.5 | |
| 27 to 31 |
| Copper (Cu), % | 0 | |
| 0 to 0.5 |
| Iron (Fe), % | 75.9 to 82.4 | |
| 2.5 to 6.0 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 1.5 to 2.5 | |
| 0 |
| Nickel (Ni), % | 4.5 to 6.5 | |
| 53.3 to 67.5 |
| Niobium (Nb), % | 0 | |
| 0.5 to 2.5 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.010 |
| Titanium (Ti), % | 0 to 0.010 | |
| 0 to 1.0 |
| Vanadium (V), % | 0.1 to 0.5 | |
| 0 |