60Cr-40Ni Alloy vs. Monel R-405
60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while Monel R-405 belongs to the nickel alloys. They have a modest 39% of their average alloy composition in common, which, by itself, doesn't mean much. There are 19 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.
For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is Monel R-405.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 220 | |
160 |
Poisson's Ratio | 0.25 | |
0.32 |
Shear Modulus, GPa | 87 | |
62 |
Tensile Strength: Ultimate (UTS), MPa | 870 | |
540 to 630 |
Tensile Strength: Yield (Proof), MPa | 660 | |
190 to 350 |
Thermal Properties
Latent Heat of Fusion, J/g | 370 | |
270 |
Specific Heat Capacity, J/kg-K | 490 | |
430 |
Thermal Expansion, µm/m-K | 16 | |
14 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 49 | |
50 |
Density, g/cm3 | 7.8 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 7.4 | |
7.9 |
Embodied Energy, MJ/kg | 110 | |
110 |
Embodied Water, L/kg | 380 | |
250 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1000 | |
120 to 370 |
Stiffness to Weight: Axial, points | 16 | |
10 |
Stiffness to Weight: Bending, points | 26 | |
21 |
Strength to Weight: Axial, points | 31 | |
17 to 20 |
Strength to Weight: Bending, points | 26 | |
17 to 18 |
Thermal Shock Resistance, points | 18 | |
17 to 20 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.3 |
Chromium (Cr), % | 58 to 62 | |
0 |
Copper (Cu), % | 0 | |
28 to 34 |
Iron (Fe), % | 0 to 1.0 | |
0 to 2.5 |
Manganese (Mn), % | 0 to 0.3 | |
0 to 2.0 |
Nickel (Ni), % | 34.5 to 42 | |
63 to 72 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
0 to 0.5 |
Sulfur (S), % | 0 to 0.020 | |
0.025 to 0.060 |
Titanium (Ti), % | 0 to 0.5 | |
0 |