60Cr-40Ni Alloy vs. EN 1.7366 Steel
60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while EN 1.7366 steel belongs to the iron alloys. There are 19 material properties with values for both materials. Properties with values for just one material (14, in this case) are not shown.
For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is EN 1.7366 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 220 | |
190 |
Poisson's Ratio | 0.25 | |
0.29 |
Shear Modulus, GPa | 87 | |
74 |
Tensile Strength: Ultimate (UTS), MPa | 870 | |
460 to 710 |
Tensile Strength: Yield (Proof), MPa | 660 | |
230 to 480 |
Thermal Properties
Latent Heat of Fusion, J/g | 370 | |
260 |
Specific Heat Capacity, J/kg-K | 490 | |
470 |
Thermal Expansion, µm/m-K | 16 | |
13 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 49 | |
4.3 |
Density, g/cm3 | 7.8 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 7.4 | |
1.7 |
Embodied Energy, MJ/kg | 110 | |
23 |
Embodied Water, L/kg | 380 | |
69 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1000 | |
140 to 600 |
Stiffness to Weight: Axial, points | 16 | |
14 |
Stiffness to Weight: Bending, points | 26 | |
25 |
Strength to Weight: Axial, points | 31 | |
16 to 25 |
Strength to Weight: Bending, points | 26 | |
17 to 23 |
Thermal Shock Resistance, points | 18 | |
13 to 20 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.18 |
Chromium (Cr), % | 58 to 62 | |
4.0 to 6.0 |
Iron (Fe), % | 0 to 1.0 | |
91.9 to 95.3 |
Manganese (Mn), % | 0 to 0.3 | |
0.3 to 0.8 |
Molybdenum (Mo), % | 0 | |
0.45 to 0.65 |
Nickel (Ni), % | 34.5 to 42 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.025 |
Silicon (Si), % | 0 to 1.0 | |
0 to 0.4 |
Sulfur (S), % | 0 to 0.020 | |
0 to 0.015 |
Titanium (Ti), % | 0 to 0.5 | |
0 |