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C18200 Copper vs. C85700 Brass

Both C18200 copper and C85700 brass are copper alloys. They have 61% 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 C18200 copper and the bottom bar is C85700 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
100
Elongation at Break, % 11 to 40
17
Poisson's Ratio 0.34
0.31
Shear Modulus, GPa 44
40
Tensile Strength: Ultimate (UTS), MPa 310 to 530
310
Tensile Strength: Yield (Proof), MPa 97 to 450
110

Thermal Properties

Latent Heat of Fusion, J/g 210
170
Maximum Temperature: Mechanical, °C 200
120
Melting Completion (Liquidus), °C 1080
940
Melting Onset (Solidus), °C 1070
910
Specific Heat Capacity, J/kg-K 390
380
Thermal Conductivity, W/m-K 320
84
Thermal Expansion, µm/m-K 18
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 80
22
Electrical Conductivity: Equal Weight (Specific), % IACS 81
25

Otherwise Unclassified Properties

Base Metal Price, % relative 31
24
Density, g/cm3 8.9
8.0
Embodied Carbon, kg CO2/kg material 2.6
2.8
Embodied Energy, MJ/kg 41
47
Embodied Water, L/kg 310
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 43 to 96
41
Resilience: Unit (Modulus of Resilience), kJ/m3 40 to 860
59
Stiffness to Weight: Axial, points 7.3
7.2
Stiffness to Weight: Bending, points 18
20
Strength to Weight: Axial, points 9.6 to 16
11
Strength to Weight: Bending, points 11 to 16
13
Thermal Diffusivity, mm2/s 93
27
Thermal Shock Resistance, points 11 to 18
10

Alloy Composition


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Aluminum (Al), % 0
0 to 0.8
Chromium (Cr), % 0.6 to 1.2
0
Copper (Cu), % 98.6 to 99.4
58 to 64
Iron (Fe), % 0 to 0.1
0 to 0.7
Lead (Pb), % 0 to 0.050
0.8 to 1.5
Nickel (Ni), % 0
0 to 1.0
Silicon (Si), % 0 to 0.1
0 to 0.050
Tin (Sn), % 0
0.5 to 1.5
Zinc (Zn), % 0
32 to 40
Residuals, % 0
0 to 1.3