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C66200 Brass vs. C18900 Copper

Both C66200 brass and C18900 copper are copper alloys. They have 90% of their average alloy composition in common.

For each property being compared, the top bar is C66200 brass and the bottom bar is C18900 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 8.0 to 15
14 to 48
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 42
43
Shear Strength, MPa 270 to 300
190 to 300
Tensile Strength: Ultimate (UTS), MPa 450 to 520
260 to 500
Tensile Strength: Yield (Proof), MPa 410 to 480
67 to 390

Thermal Properties

Latent Heat of Fusion, J/g 200
210
Maximum Temperature: Mechanical, °C 180
200
Melting Completion (Liquidus), °C 1070
1080
Melting Onset (Solidus), °C 1030
1020
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 150
130
Thermal Expansion, µm/m-K 18
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
30
Electrical Conductivity: Equal Weight (Specific), % IACS 36
30

Otherwise Unclassified Properties

Base Metal Price, % relative 29
31
Density, g/cm3 8.7
8.9
Embodied Carbon, kg CO2/kg material 2.7
2.7
Embodied Energy, MJ/kg 43
42
Embodied Water, L/kg 320
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
65 to 95
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
20 to 660
Stiffness to Weight: Axial, points 7.2
7.2
Stiffness to Weight: Bending, points 19
18
Strength to Weight: Axial, points 14 to 17
8.2 to 16
Strength to Weight: Bending, points 15 to 16
10 to 16
Thermal Diffusivity, mm2/s 45
38
Thermal Shock Resistance, points 16 to 18
9.3 to 18

Alloy Composition

Aluminum (Al), % 0
0 to 0.010
Copper (Cu), % 86.6 to 91
97.7 to 99.15
Iron (Fe), % 0 to 0.050
0
Lead (Pb), % 0 to 0.050
0 to 0.020
Manganese (Mn), % 0
0.1 to 0.3
Nickel (Ni), % 0.3 to 1.0
0
Phosphorus (P), % 0.050 to 0.2
0 to 0.050
Silicon (Si), % 0
0.15 to 0.4
Tin (Sn), % 0.2 to 0.7
0.6 to 0.9
Zinc (Zn), % 6.5 to 12.9
0 to 0.1
Residuals, % 0
0 to 0.5