C66900 Brass vs. C70620 Copper-nickel
Both C66900 brass and C70620 copper-nickel are copper alloys. They have 64% 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 C66900 brass and the bottom bar is C70620 copper-nickel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 120 | |
120 |
Poisson's Ratio | 0.32 | |
0.34 |
Rockwell B Hardness | 65 to 100 | |
65 to 87 |
Rockwell Superficial 30T Hardness | 60 to 88 | |
61 to 75 |
Shear Modulus, GPa | 45 | |
46 |
Tensile Strength: Ultimate (UTS), MPa | 460 to 770 | |
300 to 570 |
Thermal Properties
Latent Heat of Fusion, J/g | 190 | |
220 |
Maximum Temperature: Mechanical, °C | 150 | |
220 |
Melting Completion (Liquidus), °C | 860 | |
1120 |
Melting Onset (Solidus), °C | 850 | |
1060 |
Specific Heat Capacity, J/kg-K | 400 | |
390 |
Thermal Expansion, µm/m-K | 20 | |
17 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 23 | |
33 |
Density, g/cm3 | 8.2 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 2.8 | |
3.4 |
Embodied Energy, MJ/kg | 46 | |
51 |
Embodied Water, L/kg | 310 | |
300 |
Common Calculations
Stiffness to Weight: Axial, points | 8.1 | |
7.7 |
Stiffness to Weight: Bending, points | 20 | |
19 |
Strength to Weight: Axial, points | 15 to 26 | |
9.3 to 18 |
Strength to Weight: Bending, points | 16 to 23 | |
11 to 17 |
Thermal Shock Resistance, points | 14 to 23 | |
10 to 20 |
Alloy Composition
Carbon (C), % | 0 | |
0 to 0.050 |
Copper (Cu), % | 62.5 to 64.5 | |
86.5 to 90 |
Iron (Fe), % | 0 to 0.25 | |
1.0 to 1.8 |
Lead (Pb), % | 0 to 0.050 | |
0 to 0.020 |
Manganese (Mn), % | 11.5 to 12.5 | |
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), % | 22.5 to 26 | |
0 to 0.5 |
Residuals, % | 0 | |
0 to 0.5 |