60Cr-40Ni Alloy vs. EN 1.1122 Steel
60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while EN 1.1122 steel belongs to the iron alloys. There are 19 material properties with values for both materials. Properties with values for just one material (13, in this case) are not shown.
For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is EN 1.1122 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 | |
73 |
Tensile Strength: Ultimate (UTS), MPa | 870 | |
340 to 460 |
Tensile Strength: Yield (Proof), MPa | 660 | |
240 to 370 |
Thermal Properties
Latent Heat of Fusion, J/g | 370 | |
250 |
Specific Heat Capacity, J/kg-K | 490 | |
470 |
Thermal Expansion, µm/m-K | 16 | |
12 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 49 | |
1.8 |
Density, g/cm3 | 7.8 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 7.4 | |
1.4 |
Embodied Energy, MJ/kg | 110 | |
18 |
Embodied Water, L/kg | 380 | |
46 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1000 | |
160 to 360 |
Stiffness to Weight: Axial, points | 16 | |
13 |
Stiffness to Weight: Bending, points | 26 | |
24 |
Strength to Weight: Axial, points | 31 | |
12 to 16 |
Strength to Weight: Bending, points | 26 | |
14 to 17 |
Thermal Shock Resistance, points | 18 | |
11 to 15 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0.080 to 0.12 |
Chromium (Cr), % | 58 to 62 | |
0 |
Copper (Cu), % | 0 | |
0 to 0.25 |
Iron (Fe), % | 0 to 1.0 | |
98.7 to 99.62 |
Manganese (Mn), % | 0 to 0.3 | |
0.3 to 0.6 |
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 0.3 |
Sulfur (S), % | 0 to 0.020 | |
0 to 0.025 |
Titanium (Ti), % | 0 to 0.5 | |
0 |