C23400 Brass vs. C70620 Copper-nickel
Both C23400 brass and C70620 copper-nickel are copper alloys. They have 83% of their average alloy composition in common.
For each property being compared, the top bar is C23400 brass and the bottom bar is C70620 copper-nickel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
120 |
Poisson's Ratio | 0.32 | |
0.34 |
Rockwell B Hardness | 52 to 91 | |
65 to 87 |
Rockwell Superficial 30T Hardness | 51 to 78 | |
61 to 75 |
Shear Modulus, GPa | 42 | |
46 |
Tensile Strength: Ultimate (UTS), MPa | 370 to 640 | |
300 to 570 |
Thermal Properties
Latent Heat of Fusion, J/g | 190 | |
220 |
Maximum Temperature: Mechanical, °C | 160 | |
220 |
Melting Completion (Liquidus), °C | 970 | |
1120 |
Melting Onset (Solidus), °C | 930 | |
1060 |
Specific Heat Capacity, J/kg-K | 390 | |
390 |
Thermal Conductivity, W/m-K | 120 | |
49 |
Thermal Expansion, µm/m-K | 19 | |
17 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 27 | |
33 |
Density, g/cm3 | 8.5 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 2.6 | |
3.4 |
Embodied Energy, MJ/kg | 43 | |
51 |
Embodied Water, L/kg | 320 | |
300 |
Common Calculations
Stiffness to Weight: Axial, points | 7.2 | |
7.7 |
Stiffness to Weight: Bending, points | 19 | |
19 |
Strength to Weight: Axial, points | 12 to 21 | |
9.3 to 18 |
Strength to Weight: Bending, points | 13 to 19 | |
11 to 17 |
Thermal Diffusivity, mm2/s | 36 | |
14 |
Thermal Shock Resistance, points | 12 to 22 | |
10 to 20 |
Alloy Composition
Carbon (C), % | 0 | |
0 to 0.050 |
Copper (Cu), % | 81 to 84 | |
86.5 to 90 |
Iron (Fe), % | 0 to 0.050 | |
1.0 to 1.8 |
Lead (Pb), % | 0 to 0.050 | |
0 to 0.020 |
Manganese (Mn), % | 0 | |
0 to 1.0 |
Nickel (Ni), % | 0 | |
9.0 to 11 |
Phosphorus (P), % | 0 | |
0 to 0.2 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Zinc (Zn), % | 15.7 to 19 | |
0 to 0.5 |
Residuals, % | 0 | |
0 to 0.5 |