Monel R-405 vs. S66286 Stainless Steel
Monel R-405 belongs to the nickel alloys classification, while S66286 stainless steel belongs to the iron alloys. They have a modest 28% of their average alloy composition in common, which, by itself, doesn't mean much. There are 30 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 Monel R-405 and the bottom bar is S66286 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 160 | |
| 190 |
| Elongation at Break, % | 9.1 to 39 | |
| 17 to 40 |
| Fatigue Strength, MPa | 210 to 250 | |
| 240 to 410 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Shear Modulus, GPa | 62 | |
| 75 |
| Shear Strength, MPa | 350 to 370 | |
| 420 to 630 |
| Tensile Strength: Ultimate (UTS), MPa | 540 to 630 | |
| 620 to 1020 |
| Tensile Strength: Yield (Proof), MPa | 190 to 350 | |
| 280 to 670 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 300 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 920 |
| Melting Completion (Liquidus), °C | 1350 | |
| 1430 |
| Melting Onset (Solidus), °C | 1300 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 430 | |
| 470 |
| Thermal Conductivity, W/m-K | 23 | |
| 15 |
| Thermal Expansion, µm/m-K | 14 | |
| 17 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 3.4 | |
| 1.9 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.4 | |
| 2.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 50 | |
| 26 |
| Density, g/cm3 | 8.9 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 7.9 | |
| 6.0 |
| Embodied Energy, MJ/kg | 110 | |
| 87 |
| Embodied Water, L/kg | 250 | |
| 170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 49 to 170 | |
| 150 to 200 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 120 to 370 | |
| 190 to 1150 |
| Stiffness to Weight: Axial, points | 10 | |
| 14 |
| Stiffness to Weight: Bending, points | 21 | |
| 24 |
| Strength to Weight: Axial, points | 17 to 20 | |
| 22 to 36 |
| Strength to Weight: Bending, points | 17 to 18 | |
| 20 to 28 |
| Thermal Diffusivity, mm2/s | 5.9 | |
| 4.0 |
| Thermal Shock Resistance, points | 17 to 20 | |
| 13 to 22 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.35 |
| Boron (B), % | 0 | |
| 0.0010 to 0.010 |
| Carbon (C), % | 0 to 0.3 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0 | |
| 13.5 to 16 |
| Copper (Cu), % | 28 to 34 | |
| 0 |
| Iron (Fe), % | 0 to 2.5 | |
| 49.1 to 59.5 |
| Manganese (Mn), % | 0 to 2.0 | |
| 0 to 2.0 |
| Molybdenum (Mo), % | 0 | |
| 1.0 to 1.5 |
| Nickel (Ni), % | 63 to 72 | |
| 24 to 27 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 1.0 |
| Sulfur (S), % | 0.025 to 0.060 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 | |
| 1.9 to 2.4 |
| Vanadium (V), % | 0 | |
| 0.1 to 0.5 |