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C66200 Brass vs. CC140C Copper

Both C66200 brass and CC140C copper are copper alloys. They have 89% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is C66200 brass and the bottom bar is CC140C copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 8.0 to 15
11
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 42
44
Tensile Strength: Ultimate (UTS), MPa 450 to 520
340
Tensile Strength: Yield (Proof), MPa 410 to 480
230

Thermal Properties

Latent Heat of Fusion, J/g 200
210
Maximum Temperature: Mechanical, °C 180
200
Melting Completion (Liquidus), °C 1070
1100
Melting Onset (Solidus), °C 1030
1040
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 150
310
Thermal Expansion, µm/m-K 18
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
77
Electrical Conductivity: Equal Weight (Specific), % IACS 36
78

Otherwise Unclassified Properties

Base Metal Price, % relative 29
31
Density, g/cm3 8.7
8.9
Embodied Carbon, kg CO2/kg material 2.7
2.6
Embodied Energy, MJ/kg 43
41
Embodied Water, L/kg 320
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
34
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
220
Stiffness to Weight: Axial, points 7.2
7.3
Stiffness to Weight: Bending, points 19
18
Strength to Weight: Axial, points 14 to 17
10
Strength to Weight: Bending, points 15 to 16
12
Thermal Diffusivity, mm2/s 45
89
Thermal Shock Resistance, points 16 to 18
12

Alloy Composition

Chromium (Cr), % 0
0.4 to 1.2
Copper (Cu), % 86.6 to 91
98.8 to 99.6
Iron (Fe), % 0 to 0.050
0
Lead (Pb), % 0 to 0.050
0
Nickel (Ni), % 0.3 to 1.0
0
Phosphorus (P), % 0.050 to 0.2
0
Tin (Sn), % 0.2 to 0.7
0
Zinc (Zn), % 6.5 to 12.9
0
Residuals, % 0 to 0.5
0