Monel K-500 vs. Nickel 625
Both Monel K-500 and nickel 625 are nickel alloys. They have 65% of their average alloy composition in common. There are 31 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 Monel K-500 and the bottom bar is nickel 625.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 160 | |
200 |
Elongation at Break, % | 25 to 36 | |
33 to 34 |
Fatigue Strength, MPa | 260 to 560 | |
240 to 320 |
Poisson's Ratio | 0.32 | |
0.29 |
Shear Modulus, GPa | 61 | |
79 |
Shear Strength, MPa | 430 to 700 | |
530 to 600 |
Tensile Strength: Ultimate (UTS), MPa | 640 to 1100 | |
790 to 910 |
Tensile Strength: Yield (Proof), MPa | 310 to 880 | |
320 to 450 |
Thermal Properties
Curie Temperature, °C | -67 | |
-200 |
Latent Heat of Fusion, J/g | 270 | |
330 |
Maximum Temperature: Mechanical, °C | 900 | |
980 |
Melting Completion (Liquidus), °C | 1350 | |
1350 |
Melting Onset (Solidus), °C | 1320 | |
1290 |
Specific Heat Capacity, J/kg-K | 440 | |
440 |
Thermal Conductivity, W/m-K | 18 | |
11 |
Thermal Expansion, µm/m-K | 14 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 3.1 | |
1.3 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 3.2 | |
1.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 50 | |
80 |
Density, g/cm3 | 8.7 | |
8.6 |
Embodied Carbon, kg CO2/kg material | 8.1 | |
14 |
Embodied Energy, MJ/kg | 120 | |
190 |
Embodied Water, L/kg | 280 | |
290 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 180 to 260 | |
220 to 250 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 300 to 2420 | |
260 to 490 |
Stiffness to Weight: Axial, points | 10 | |
13 |
Stiffness to Weight: Bending, points | 21 | |
23 |
Strength to Weight: Axial, points | 21 to 35 | |
26 to 29 |
Strength to Weight: Bending, points | 19 to 27 | |
22 to 24 |
Thermal Diffusivity, mm2/s | 4.8 | |
2.9 |
Thermal Shock Resistance, points | 21 to 36 | |
22 to 25 |
Alloy Composition
Aluminum (Al), % | 2.3 to 3.2 | |
0 to 0.4 |
Carbon (C), % | 0 to 0.18 | |
0 to 0.1 |
Chromium (Cr), % | 0 | |
20 to 23 |
Cobalt (Co), % | 0 | |
0 to 1.0 |
Copper (Cu), % | 27 to 33 | |
0 |
Iron (Fe), % | 0 to 2.0 | |
0 to 5.0 |
Manganese (Mn), % | 0 to 1.5 | |
0 to 0.5 |
Molybdenum (Mo), % | 0 | |
8.0 to 10 |
Nickel (Ni), % | 63 to 70.4 | |
58 to 68.9 |
Niobium (Nb), % | 0 | |
3.2 to 4.2 |
Phosphorus (P), % | 0 | |
0 to 0.015 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.5 |
Sulfur (S), % | 0 to 0.010 | |
0 to 0.015 |
Titanium (Ti), % | 0.35 to 0.85 | |
0 to 0.4 |