EN 1.5525 Steel vs. 60Cr-40Ni Alloy
EN 1.5525 steel belongs to the iron alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. 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 EN 1.5525 steel and the bottom bar is 60Cr-40Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
220 |
Poisson's Ratio | 0.29 | |
0.25 |
Shear Modulus, GPa | 73 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 440 to 1440 | |
870 |
Tensile Strength: Yield (Proof), MPa | 300 to 490 | |
660 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
370 |
Specific Heat Capacity, J/kg-K | 470 | |
490 |
Thermal Expansion, µm/m-K | 13 | |
16 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 1.9 | |
49 |
Density, g/cm3 | 7.8 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 1.4 | |
7.4 |
Embodied Energy, MJ/kg | 19 | |
110 |
Embodied Water, L/kg | 48 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 240 to 640 | |
1000 |
Stiffness to Weight: Axial, points | 13 | |
16 |
Stiffness to Weight: Bending, points | 24 | |
26 |
Strength to Weight: Axial, points | 16 to 51 | |
31 |
Strength to Weight: Bending, points | 16 to 36 | |
26 |
Thermal Shock Resistance, points | 13 to 42 | |
18 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.25 |
Boron (B), % | 0.00080 to 0.0050 | |
0 |
Carbon (C), % | 0.18 to 0.23 | |
0 to 0.1 |
Chromium (Cr), % | 0 to 0.3 | |
58 to 62 |
Copper (Cu), % | 0 to 0.25 | |
0 |
Iron (Fe), % | 97.7 to 98.9 | |
0 to 1.0 |
Manganese (Mn), % | 0.9 to 1.2 | |
0 to 0.3 |
Nickel (Ni), % | 0 | |
34.5 to 42 |
Nitrogen (N), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.025 | |
0 to 0.020 |
Silicon (Si), % | 0 to 0.3 | |
0 to 1.0 |
Sulfur (S), % | 0 to 0.025 | |
0 to 0.020 |
Titanium (Ti), % | 0 | |
0 to 0.5 |