C68000 Brass vs. C71500 Copper-nickel
Both C68000 brass and C71500 copper-nickel are copper alloys. They have 60% 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 C68000 brass and the bottom bar is C71500 copper-nickel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 100 | |
140 |
Poisson's Ratio | 0.3 | |
0.33 |
Shear Modulus, GPa | 40 | |
52 |
Tensile Strength: Ultimate (UTS), MPa | 390 | |
380 to 620 |
Thermal Properties
Latent Heat of Fusion, J/g | 170 | |
230 |
Maximum Temperature: Mechanical, °C | 120 | |
260 |
Melting Completion (Liquidus), °C | 880 | |
1240 |
Melting Onset (Solidus), °C | 870 | |
1170 |
Specific Heat Capacity, J/kg-K | 390 | |
400 |
Thermal Conductivity, W/m-K | 96 | |
28 |
Thermal Expansion, µm/m-K | 21 | |
16 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 23 | |
41 |
Density, g/cm3 | 8.0 | |
8.9 |
Embodied Carbon, kg CO2/kg material | 2.8 | |
5.1 |
Embodied Energy, MJ/kg | 48 | |
74 |
Embodied Water, L/kg | 330 | |
280 |
Common Calculations
Stiffness to Weight: Axial, points | 7.3 | |
8.6 |
Stiffness to Weight: Bending, points | 20 | |
19 |
Strength to Weight: Axial, points | 14 | |
12 to 19 |
Strength to Weight: Bending, points | 15 | |
13 to 18 |
Thermal Diffusivity, mm2/s | 31 | |
7.7 |
Thermal Shock Resistance, points | 13 | |
12 to 20 |
Alloy Composition
Aluminum (Al), % | 0 to 0.010 | |
0 |
Copper (Cu), % | 56 to 60 | |
63.5 to 70.6 |
Iron (Fe), % | 0.25 to 1.3 | |
0.4 to 1.0 |
Lead (Pb), % | 0 to 0.050 | |
0 to 0.050 |
Manganese (Mn), % | 0.010 to 0.5 | |
0 to 1.0 |
Nickel (Ni), % | 0.2 to 0.8 | |
29 to 33 |
Silicon (Si), % | 0.040 to 0.15 | |
0 |
Tin (Sn), % | 0.75 to 1.1 | |
0 |
Zinc (Zn), % | 35.6 to 42.8 | |
0 to 1.0 |
Residuals, % | 0 | |
0 to 0.5 |