EN 1.4110 Stainless Steel vs. Nickel 908
EN 1.4110 stainless steel belongs to the iron alloys classification, while nickel 908 belongs to the nickel alloys. They have 45% of their average alloy composition in common. There are 29 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 EN 1.4110 stainless steel and the bottom bar is nickel 908.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 180 |
| Elongation at Break, % | 11 to 14 | |
| 11 |
| Fatigue Strength, MPa | 250 to 730 | |
| 450 |
| Poisson's Ratio | 0.28 | |
| 0.3 |
| Shear Modulus, GPa | 76 | |
| 70 |
| Shear Strength, MPa | 470 to 1030 | |
| 800 |
| Tensile Strength: Ultimate (UTS), MPa | 770 to 1720 | |
| 1340 |
| Tensile Strength: Yield (Proof), MPa | 430 to 1330 | |
| 930 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 790 | |
| 920 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1430 |
| Melting Onset (Solidus), °C | 1400 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 460 |
| Thermal Conductivity, W/m-K | 30 | |
| 11 |
| Thermal Expansion, µm/m-K | 11 | |
| 8.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 8.0 | |
| 50 |
| Density, g/cm3 | 7.7 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 2.3 | |
| 9.3 |
| Embodied Energy, MJ/kg | 33 | |
| 140 |
| Embodied Water, L/kg | 110 | |
| 170 |
Common Calculations
| PREN (Pitting Resistance) | 16 | |
| 4.2 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 90 to 180 | |
| 140 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 480 to 4550 | |
| 2340 |
| Stiffness to Weight: Axial, points | 14 | |
| 12 |
| Stiffness to Weight: Bending, points | 25 | |
| 23 |
| Strength to Weight: Axial, points | 28 to 62 | |
| 45 |
| Strength to Weight: Bending, points | 24 to 41 | |
| 33 |
| Thermal Diffusivity, mm2/s | 8.1 | |
| 2.9 |
| Thermal Shock Resistance, points | 27 to 60 | |
| 61 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0.75 to 1.3 |
| Boron (B), % | 0 | |
| 0 to 0.012 |
| Carbon (C), % | 0.48 to 0.6 | |
| 0 to 0.030 |
| Chromium (Cr), % | 13 to 15 | |
| 3.8 to 4.5 |
| Cobalt (Co), % | 0 | |
| 0 to 0.5 |
| Copper (Cu), % | 0 | |
| 0 to 0.5 |
| Iron (Fe), % | 81.4 to 86 | |
| 35.6 to 44.6 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0.5 to 0.8 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 47 to 51 |
| Niobium (Nb), % | 0 | |
| 2.7 to 3.3 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.015 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.0050 |
| Titanium (Ti), % | 0 | |
| 1.2 to 1.8 |
| Vanadium (V), % | 0 to 0.15 | |
| 0 |