C55180 Copper vs. C99750 Brass
Both C55180 copper and C99750 brass are copper alloys. They have 58% of their average alloy composition in common. There are 24 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.
For each property being compared, the top bar is C55180 copper and the bottom bar is C99750 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
130 |
Elongation at Break, % | 20 | |
20 to 30 |
Poisson's Ratio | 0.34 | |
0.32 |
Shear Modulus, GPa | 41 | |
48 |
Tensile Strength: Ultimate (UTS), MPa | 200 | |
450 to 520 |
Tensile Strength: Yield (Proof), MPa | 100 | |
220 to 280 |
Thermal Properties
Latent Heat of Fusion, J/g | 200 | |
200 |
Maximum Temperature: Mechanical, °C | 200 | |
160 |
Melting Completion (Liquidus), °C | 920 | |
840 |
Melting Onset (Solidus), °C | 710 | |
820 |
Specific Heat Capacity, J/kg-K | 400 | |
410 |
Thermal Expansion, µm/m-K | 17 | |
20 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 29 | |
23 |
Density, g/cm3 | 8.6 | |
8.1 |
Embodied Carbon, kg CO2/kg material | 2.5 | |
3.1 |
Embodied Energy, MJ/kg | 39 | |
51 |
Embodied Water, L/kg | 290 | |
310 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 34 | |
87 to 110 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 48 | |
190 to 300 |
Stiffness to Weight: Axial, points | 7.1 | |
8.6 |
Stiffness to Weight: Bending, points | 18 | |
21 |
Strength to Weight: Axial, points | 6.4 | |
15 to 18 |
Strength to Weight: Bending, points | 8.8 | |
16 to 18 |
Thermal Shock Resistance, points | 7.9 | |
13 to 15 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.25 to 3.0 |
Copper (Cu), % | 94.7 to 95.2 | |
55 to 61 |
Iron (Fe), % | 0 | |
0 to 1.0 |
Lead (Pb), % | 0 | |
0.5 to 2.5 |
Manganese (Mn), % | 0 | |
17 to 23 |
Nickel (Ni), % | 0 | |
0 to 5.0 |
Phosphorus (P), % | 4.8 to 5.2 | |
0 |
Zinc (Zn), % | 0 | |
17 to 23 |
Residuals, % | 0 | |
0 to 0.3 |