Monel K-500 vs. S20910 Stainless Steel
Monel K-500 belongs to the nickel alloys classification, while S20910 stainless steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.
For each property being compared, the top bar is Monel K-500 and the bottom bar is S20910 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 160 | |
| 200 |
| Elongation at Break, % | 25 to 36 | |
| 14 to 39 |
| Fatigue Strength, MPa | 260 to 560 | |
| 310 to 460 |
| Poisson's Ratio | 0.32 | |
| 0.28 |
| Shear Modulus, GPa | 61 | |
| 79 |
| Shear Strength, MPa | 430 to 700 | |
| 500 to 570 |
| Tensile Strength: Ultimate (UTS), MPa | 640 to 1100 | |
| 780 to 940 |
| Tensile Strength: Yield (Proof), MPa | 310 to 880 | |
| 430 to 810 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 300 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 1080 |
| Melting Completion (Liquidus), °C | 1350 | |
| 1420 |
| Melting Onset (Solidus), °C | 1320 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 480 |
| Thermal Conductivity, W/m-K | 18 | |
| 13 |
| Thermal Expansion, µm/m-K | 14 | |
| 16 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 50 | |
| 22 |
| Density, g/cm3 | 8.7 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.1 | |
| 4.8 |
| Embodied Energy, MJ/kg | 120 | |
| 68 |
| Embodied Water, L/kg | 280 | |
| 180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 180 to 260 | |
| 120 to 260 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 300 to 2420 | |
| 460 to 1640 |
| Stiffness to Weight: Axial, points | 10 | |
| 14 |
| Stiffness to Weight: Bending, points | 21 | |
| 25 |
| Strength to Weight: Axial, points | 21 to 35 | |
| 28 to 33 |
| Strength to Weight: Bending, points | 19 to 27 | |
| 24 to 27 |
| Thermal Diffusivity, mm2/s | 4.8 | |
| 3.6 |
| Thermal Shock Resistance, points | 21 to 36 | |
| 17 to 21 |
Alloy Composition
| Aluminum (Al), % | 2.3 to 3.2 | |
| 0 |
| Carbon (C), % | 0 to 0.18 | |
| 0 to 0.060 |
| Chromium (Cr), % | 0 | |
| 20.5 to 23.5 |
| Copper (Cu), % | 27 to 33 | |
| 0 |
| Iron (Fe), % | 0 to 2.0 | |
| 52.1 to 62.1 |
| Manganese (Mn), % | 0 to 1.5 | |
| 4.0 to 6.0 |
| Molybdenum (Mo), % | 0 | |
| 1.5 to 3.0 |
| Nickel (Ni), % | 63 to 70.4 | |
| 11.5 to 13.5 |
| Niobium (Nb), % | 0 | |
| 0.1 to 0.3 |
| Nitrogen (N), % | 0 | |
| 0.2 to 0.4 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0.35 to 0.85 | |
| 0 |
| Vanadium (V), % | 0 | |
| 0.1 to 0.3 |