C23400 Brass vs. C66900 Brass
Both C23400 brass and C66900 brass are copper alloys. They have 81% of their average alloy composition in common. There are 22 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.
For each property being compared, the top bar is C23400 brass and the bottom bar is C66900 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
120 |
Poisson's Ratio | 0.32 | |
0.32 |
Rockwell B Hardness | 52 to 91 | |
65 to 100 |
Rockwell Superficial 30T Hardness | 51 to 78 | |
60 to 88 |
Shear Modulus, GPa | 42 | |
45 |
Tensile Strength: Ultimate (UTS), MPa | 370 to 640 | |
460 to 770 |
Thermal Properties
Latent Heat of Fusion, J/g | 190 | |
190 |
Maximum Temperature: Mechanical, °C | 160 | |
150 |
Melting Completion (Liquidus), °C | 970 | |
860 |
Melting Onset (Solidus), °C | 930 | |
850 |
Specific Heat Capacity, J/kg-K | 390 | |
400 |
Thermal Expansion, µm/m-K | 19 | |
20 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 27 | |
23 |
Density, g/cm3 | 8.5 | |
8.2 |
Embodied Carbon, kg CO2/kg material | 2.6 | |
2.8 |
Embodied Energy, MJ/kg | 43 | |
46 |
Embodied Water, L/kg | 320 | |
310 |
Common Calculations
Stiffness to Weight: Axial, points | 7.2 | |
8.1 |
Stiffness to Weight: Bending, points | 19 | |
20 |
Strength to Weight: Axial, points | 12 to 21 | |
15 to 26 |
Strength to Weight: Bending, points | 13 to 19 | |
16 to 23 |
Thermal Shock Resistance, points | 12 to 22 | |
14 to 23 |
Alloy Composition
Copper (Cu), % | 81 to 84 | |
62.5 to 64.5 |
Iron (Fe), % | 0 to 0.050 | |
0 to 0.25 |
Lead (Pb), % | 0 to 0.050 | |
0 to 0.050 |
Manganese (Mn), % | 0 | |
11.5 to 12.5 |
Zinc (Zn), % | 15.7 to 19 | |
22.5 to 26 |
Residuals, % | 0 | |
0 to 0.2 |