Hot Worked Monel K-500 vs. Hot Worked Nickel 200
Both hot worked Monel K-500 and hot worked nickel 200 are nickel alloys. Both are furnished in the hot worked condition. They have 67% of their average alloy composition in common. There are 32 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is hot worked Monel K-500 and the bottom bar is hot worked nickel 200.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 160 | |
| 180 |
| Elongation at Break, % | 36 | |
| 42 |
| Fatigue Strength, MPa | 300 | |
| 120 |
| Poisson's Ratio | 0.32 | |
| 0.31 |
| Shear Modulus, GPa | 61 | |
| 70 |
| Shear Strength, MPa | 520 | |
| 330 |
| Tensile Strength: Ultimate (UTS), MPa | 770 | |
| 480 |
| Tensile Strength: Yield (Proof), MPa | 410 | |
| 150 |
Thermal Properties
| Curie Temperature, °C | -67 | |
| 360 |
| Latent Heat of Fusion, J/g | 270 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 900 |
| Melting Completion (Liquidus), °C | 1350 | |
| 1460 |
| Melting Onset (Solidus), °C | 1320 | |
| 1440 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 450 |
| Thermal Conductivity, W/m-K | 18 | |
| 69 |
| Thermal Expansion, µm/m-K | 14 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 3.1 | |
| 18 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.2 | |
| 18 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 50 | |
| 65 |
| Calomel Potential, mV | -100 | |
| -150 |
| Density, g/cm3 | 8.7 | |
| 8.9 |
| Embodied Carbon, kg CO2/kg material | 8.1 | |
| 11 |
| Embodied Energy, MJ/kg | 120 | |
| 150 |
| Embodied Water, L/kg | 280 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 240 | |
| 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 530 | |
| 58 |
| Stiffness to Weight: Axial, points | 10 | |
| 11 |
| Stiffness to Weight: Bending, points | 21 | |
| 21 |
| Strength to Weight: Axial, points | 25 | |
| 15 |
| Strength to Weight: Bending, points | 22 | |
| 15 |
| Thermal Diffusivity, mm2/s | 4.8 | |
| 17 |
| Thermal Shock Resistance, points | 25 | |
| 14 |
Alloy Composition
| Aluminum (Al), % | 2.3 to 3.2 | |
| 0 |
| Carbon (C), % | 0 to 0.18 | |
| 0 to 0.15 |
| Copper (Cu), % | 27 to 33 | |
| 0 to 0.25 |
| Iron (Fe), % | 0 to 2.0 | |
| 0 to 0.4 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 0.35 |
| Nickel (Ni), % | 63 to 70.4 | |
| 99 to 100 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.35 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 to 0.010 |
| Titanium (Ti), % | 0.35 to 0.85 | |
| 0 |