C66900 Brass vs. SAE-AISI M10 Steel
C66900 brass belongs to the copper alloys classification, while SAE-AISI M10 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 C66900 brass and the bottom bar is SAE-AISI M10 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 120 | |
200 |
Poisson's Ratio | 0.32 | |
0.29 |
Shear Modulus, GPa | 45 | |
76 |
Tensile Strength: Ultimate (UTS), MPa | 460 to 770 | |
740 to 2170 |
Thermal Properties
Latent Heat of Fusion, J/g | 190 | |
270 |
Melting Completion (Liquidus), °C | 860 | |
1520 |
Melting Onset (Solidus), °C | 850 | |
1470 |
Specific Heat Capacity, J/kg-K | 400 | |
460 |
Thermal Expansion, µm/m-K | 20 | |
12 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 23 | |
14 |
Density, g/cm3 | 8.2 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 2.8 | |
8.3 |
Embodied Energy, MJ/kg | 46 | |
120 |
Embodied Water, L/kg | 310 | |
100 |
Common Calculations
Stiffness to Weight: Axial, points | 8.1 | |
14 |
Stiffness to Weight: Bending, points | 20 | |
24 |
Strength to Weight: Axial, points | 15 to 26 | |
26 to 76 |
Strength to Weight: Bending, points | 16 to 23 | |
23 to 47 |
Thermal Shock Resistance, points | 14 to 23 | |
23 to 68 |
Alloy Composition
Carbon (C), % | 0 | |
0.84 to 1.1 |
Chromium (Cr), % | 0 | |
3.8 to 4.5 |
Copper (Cu), % | 62.5 to 64.5 | |
0 to 0.25 |
Iron (Fe), % | 0 to 0.25 | |
82.3 to 85.6 |
Lead (Pb), % | 0 to 0.050 | |
0 |
Manganese (Mn), % | 11.5 to 12.5 | |
0.1 to 0.4 |
Molybdenum (Mo), % | 0 | |
7.8 to 8.5 |
Nickel (Ni), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 | |
0 to 0.030 |
Silicon (Si), % | 0 | |
0.2 to 0.45 |
Sulfur (S), % | 0 | |
0 to 0.030 |
Vanadium (V), % | 0 | |
1.8 to 2.2 |
Zinc (Zn), % | 22.5 to 26 | |
0 |
Residuals, % | 0 to 0.2 | |
0 |