C72200 Copper-nickel vs. C99600 Bronze
Both C72200 copper-nickel and C99600 bronze are copper alloys. They have 56% of their average alloy composition in common. There are 20 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.
For each property being compared, the top bar is C72200 copper-nickel and the bottom bar is C99600 bronze.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 130 | |
150 |
Poisson's Ratio | 0.33 | |
0.34 |
Shear Modulus, GPa | 48 | |
56 |
Tensile Strength: Ultimate (UTS), MPa | 350 to 580 | |
560 |
Thermal Properties
Latent Heat of Fusion, J/g | 220 | |
240 |
Maximum Temperature: Mechanical, °C | 230 | |
200 |
Melting Completion (Liquidus), °C | 1180 | |
1100 |
Melting Onset (Solidus), °C | 1120 | |
1050 |
Specific Heat Capacity, J/kg-K | 400 | |
440 |
Thermal Expansion, µm/m-K | 16 | |
19 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
22 |
Density, g/cm3 | 8.9 | |
8.1 |
Embodied Carbon, kg CO2/kg material | 3.9 | |
3.2 |
Embodied Energy, MJ/kg | 59 | |
51 |
Embodied Water, L/kg | 300 | |
300 |
Common Calculations
Stiffness to Weight: Axial, points | 8.0 | |
10 |
Stiffness to Weight: Bending, points | 19 | |
22 |
Strength to Weight: Axial, points | 11 to 18 | |
19 |
Strength to Weight: Bending, points | 12 to 17 | |
19 |
Thermal Shock Resistance, points | 12 to 20 | |
14 |
Alloy Composition
Aluminum (Al), % | 0 | |
1.0 to 2.8 |
Carbon (C), % | 0 | |
0 to 0.050 |
Chromium (Cr), % | 0.3 to 0.7 | |
0 |
Cobalt (Co), % | 0 | |
0 to 0.2 |
Copper (Cu), % | 78.1 to 84.2 | |
50.8 to 60 |
Iron (Fe), % | 0.5 to 1.0 | |
0 to 0.2 |
Lead (Pb), % | 0 to 0.050 | |
0 to 0.020 |
Manganese (Mn), % | 0 to 1.0 | |
39 to 45 |
Nickel (Ni), % | 15 to 18 | |
0 to 0.2 |
Silicon (Si), % | 0 | |
0 to 0.1 |
Tin (Sn), % | 0 | |
0 to 0.1 |
Zinc (Zn), % | 0 to 1.0 | |
0 to 0.2 |
Residuals, % | 0 | |
0 to 0.3 |