Nickel 718 vs. S36200 Stainless Steel
Nickel 718 belongs to the nickel alloys classification, while S36200 stainless steel belongs to the iron alloys. They have 40% of their average alloy composition in common. There are 31 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 nickel 718 and the bottom bar is S36200 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 190 |
| Elongation at Break, % | 12 to 50 | |
| 3.4 to 4.6 |
| Fatigue Strength, MPa | 460 to 760 | |
| 450 to 570 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Rockwell C Hardness | 40 | |
| 25 to 33 |
| Shear Modulus, GPa | 75 | |
| 76 |
| Shear Strength, MPa | 660 to 950 | |
| 680 to 810 |
| Tensile Strength: Ultimate (UTS), MPa | 930 to 1530 | |
| 1180 to 1410 |
| Tensile Strength: Yield (Proof), MPa | 510 to 1330 | |
| 960 to 1240 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 980 | |
| 820 |
| Melting Completion (Liquidus), °C | 1340 | |
| 1440 |
| Melting Onset (Solidus), °C | 1260 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 480 |
| Thermal Conductivity, W/m-K | 11 | |
| 16 |
| Thermal Expansion, µm/m-K | 13 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.4 | |
| 2.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.5 | |
| 2.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 75 | |
| 12 |
| Density, g/cm3 | 8.3 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 13 | |
| 2.8 |
| Embodied Energy, MJ/kg | 190 | |
| 40 |
| Embodied Water, L/kg | 250 | |
| 120 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 390 | |
| 46 to 51 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 660 to 4560 | |
| 2380 to 3930 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 23 | |
| 25 |
| Strength to Weight: Axial, points | 31 to 51 | |
| 42 to 50 |
| Strength to Weight: Bending, points | 25 to 35 | |
| 32 to 36 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 4.3 |
| Thermal Shock Resistance, points | 27 to 44 | |
| 40 to 48 |
Alloy Composition
| Aluminum (Al), % | 0.2 to 0.8 | |
| 0 to 0.1 |
| Boron (B), % | 0 to 0.0060 | |
| 0 |
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.050 |
| Chromium (Cr), % | 17 to 21 | |
| 14 to 14.5 |
| Cobalt (Co), % | 0 to 1.0 | |
| 0 |
| Copper (Cu), % | 0 to 0.3 | |
| 0 |
| Iron (Fe), % | 11.1 to 24.6 | |
| 75.4 to 79.5 |
| Manganese (Mn), % | 0 to 0.35 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 2.8 to 3.3 | |
| 0 to 0.3 |
| Nickel (Ni), % | 50 to 55 | |
| 6.5 to 7.0 |
| Niobium (Nb), % | 4.8 to 5.5 | |
| 0 |
| Phosphorus (P), % | 0 to 0.015 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 to 0.35 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0.65 to 1.2 | |
| 0.6 to 0.9 |