SAE-AISI 5140 Steel vs. 60Cr-40Ni Alloy
SAE-AISI 5140 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 (12, in this case) are not shown.
For each property being compared, the top bar is SAE-AISI 5140 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 | 560 to 970 | |
870 |
Tensile Strength: Yield (Proof), MPa | 290 to 840 | |
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 | 2.1 | |
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 | 49 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 220 to 1880 | |
1000 |
Stiffness to Weight: Axial, points | 13 | |
16 |
Stiffness to Weight: Bending, points | 24 | |
26 |
Strength to Weight: Axial, points | 20 to 34 | |
31 |
Strength to Weight: Bending, points | 19 to 28 | |
26 |
Thermal Shock Resistance, points | 16 to 29 | |
18 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.25 |
Carbon (C), % | 0.38 to 0.43 | |
0 to 0.1 |
Chromium (Cr), % | 0.7 to 0.9 | |
58 to 62 |
Iron (Fe), % | 97.3 to 98.1 | |
0 to 1.0 |
Manganese (Mn), % | 0.7 to 0.9 | |
0 to 0.3 |
Nickel (Ni), % | 0 | |
34.5 to 42 |
Nitrogen (N), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.035 | |
0 to 0.020 |
Silicon (Si), % | 0.15 to 0.35 | |
0 to 1.0 |
Sulfur (S), % | 0 to 0.040 | |
0 to 0.020 |
Titanium (Ti), % | 0 | |
0 to 0.5 |