SAE-AISI M62 Steel vs. C36000 Brass
SAE-AISI M62 steel belongs to the iron alloys classification, while C36000 brass belongs to the copper alloys. There are 19 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.
For each property being compared, the top bar is SAE-AISI M62 steel and the bottom bar is C36000 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
100 |
Poisson's Ratio | 0.29 | |
0.31 |
Shear Modulus, GPa | 79 | |
39 |
Tensile Strength: Ultimate (UTS), MPa | 830 to 2440 | |
330 to 530 |
Thermal Properties
Latent Heat of Fusion, J/g | 260 | |
170 |
Melting Completion (Liquidus), °C | 1650 | |
900 |
Melting Onset (Solidus), °C | 1600 | |
890 |
Specific Heat Capacity, J/kg-K | 430 | |
380 |
Thermal Expansion, µm/m-K | 12 | |
21 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 30 | |
23 |
Density, g/cm3 | 8.5 | |
8.2 |
Embodied Carbon, kg CO2/kg material | 10 | |
2.6 |
Embodied Energy, MJ/kg | 150 | |
45 |
Embodied Water, L/kg | 110 | |
320 |
Common Calculations
Stiffness to Weight: Axial, points | 13 | |
7.0 |
Stiffness to Weight: Bending, points | 23 | |
19 |
Strength to Weight: Axial, points | 27 to 80 | |
11 to 18 |
Strength to Weight: Bending, points | 23 to 47 | |
13 to 18 |
Thermal Shock Resistance, points | 24 to 71 | |
11 to 18 |
Alloy Composition
Carbon (C), % | 1.3 to 1.4 | |
0 |
Chromium (Cr), % | 3.5 to 4.0 | |
0 |
Copper (Cu), % | 0 to 0.25 | |
60 to 63 |
Iron (Fe), % | 73.6 to 77.4 | |
0 to 0.35 |
Lead (Pb), % | 0 | |
2.5 to 3.7 |
Manganese (Mn), % | 0.15 to 0.4 | |
0 |
Molybdenum (Mo), % | 10 to 11 | |
0 |
Nickel (Ni), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.030 | |
0 |
Silicon (Si), % | 0.15 to 0.4 | |
0 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Tungsten (W), % | 5.8 to 6.5 | |
0 |
Vanadium (V), % | 1.8 to 2.1 | |
0 |
Zinc (Zn), % | 0 | |
32.5 to 37.5 |
Residuals, % | 0 | |
0 to 0.5 |