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