Annealed SAE-AISI 4140 vs. Annealed SAE-AISI M62
Both annealed SAE-AISI 4140 and annealed SAE-AISI M62 are iron alloys. Both are furnished in the annealed condition. They have 78% of their average alloy composition in common. There are 20 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 annealed SAE-AISI 4140 and the bottom bar is annealed SAE-AISI M62.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 200 | |
250 |
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
200 |
Poisson's Ratio | 0.29 | |
0.29 |
Shear Modulus, GPa | 73 | |
79 |
Tensile Strength: Ultimate (UTS), MPa | 740 | |
830 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
260 |
Melting Completion (Liquidus), °C | 1460 | |
1650 |
Melting Onset (Solidus), °C | 1420 | |
1600 |
Specific Heat Capacity, J/kg-K | 470 | |
430 |
Thermal Expansion, µm/m-K | 13 | |
12 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 2.4 | |
30 |
Density, g/cm3 | 7.8 | |
8.5 |
Embodied Carbon, kg CO2/kg material | 1.5 | |
10 |
Embodied Energy, MJ/kg | 20 | |
150 |
Embodied Water, L/kg | 51 | |
110 |
Common Calculations
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 24 | |
23 |
Strength to Weight: Axial, points | 26 | |
27 |
Strength to Weight: Bending, points | 23 | |
23 |
Thermal Shock Resistance, points | 22 | |
24 |
Alloy Composition
Carbon (C), % | 0.38 to 0.43 | |
1.3 to 1.4 |
Chromium (Cr), % | 0.8 to 1.1 | |
3.5 to 4.0 |
Copper (Cu), % | 0 | |
0 to 0.25 |
Iron (Fe), % | 96.8 to 97.8 | |
73.6 to 77.4 |
Manganese (Mn), % | 0.75 to 1.0 | |
0.15 to 0.4 |
Molybdenum (Mo), % | 0.15 to 0.25 | |
10 to 11 |
Nickel (Ni), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.035 | |
0 to 0.030 |
Silicon (Si), % | 0.15 to 0.35 | |
0.15 to 0.4 |
Sulfur (S), % | 0 to 0.040 | |
0 to 0.030 |
Tungsten (W), % | 0 | |
5.8 to 6.5 |
Vanadium (V), % | 0 | |
1.8 to 2.1 |