EN 1.4606 Stainless Steel vs. Monel K-500
EN 1.4606 stainless steel belongs to the iron alloys classification, while Monel K-500 belongs to the nickel 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 (4, in this case) are not shown.
For each property being compared, the top bar is EN 1.4606 stainless steel and the bottom bar is Monel K-500.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 160 |
| Elongation at Break, % | 23 to 39 | |
| 25 to 36 |
| Fatigue Strength, MPa | 240 to 420 | |
| 260 to 560 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Shear Modulus, GPa | 75 | |
| 61 |
| Shear Strength, MPa | 410 to 640 | |
| 430 to 700 |
| Tensile Strength: Ultimate (UTS), MPa | 600 to 1020 | |
| 640 to 1100 |
| Tensile Strength: Yield (Proof), MPa | 280 to 630 | |
| 310 to 880 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 270 |
| Maximum Temperature: Mechanical, °C | 910 | |
| 900 |
| Melting Completion (Liquidus), °C | 1430 | |
| 1350 |
| Melting Onset (Solidus), °C | 1380 | |
| 1320 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 440 |
| Thermal Conductivity, W/m-K | 14 | |
| 18 |
| Thermal Expansion, µm/m-K | 11 | |
| 14 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.9 | |
| 3.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.2 | |
| 3.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 26 | |
| 50 |
| Density, g/cm3 | 7.9 | |
| 8.7 |
| Embodied Carbon, kg CO2/kg material | 6.0 | |
| 8.1 |
| Embodied Energy, MJ/kg | 87 | |
| 120 |
| Embodied Water, L/kg | 170 | |
| 280 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 190 to 200 | |
| 180 to 260 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 200 to 1010 | |
| 300 to 2420 |
| Stiffness to Weight: Axial, points | 14 | |
| 10 |
| Stiffness to Weight: Bending, points | 24 | |
| 21 |
| Strength to Weight: Axial, points | 21 to 36 | |
| 21 to 35 |
| Strength to Weight: Bending, points | 20 to 28 | |
| 19 to 27 |
| Thermal Diffusivity, mm2/s | 3.7 | |
| 4.8 |
| Thermal Shock Resistance, points | 21 to 35 | |
| 21 to 36 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.35 | |
| 2.3 to 3.2 |
| Boron (B), % | 0.0010 to 0.010 | |
| 0 |
| Carbon (C), % | 0 to 0.080 | |
| 0 to 0.18 |
| Chromium (Cr), % | 13 to 16 | |
| 0 |
| Copper (Cu), % | 0 | |
| 27 to 33 |
| Iron (Fe), % | 49.2 to 59 | |
| 0 to 2.0 |
| Manganese (Mn), % | 1.0 to 2.0 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 1.0 to 1.5 | |
| 0 |
| Nickel (Ni), % | 24 to 27 | |
| 63 to 70.4 |
| Phosphorus (P), % | 0 to 0.025 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.010 |
| Titanium (Ti), % | 1.9 to 2.3 | |
| 0.35 to 0.85 |
| Vanadium (V), % | 0.1 to 0.5 | |
| 0 |