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C19800 Copper vs. C66200 Brass

Both C19800 copper and C66200 brass are copper alloys. They have a moderately high 90% of their average alloy composition in common.

For each property being compared, the top bar is C19800 copper and the bottom bar is C66200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 9.0 to 12
8.0 to 15
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 43
42
Shear Strength, MPa 260 to 330
270 to 300
Tensile Strength: Ultimate (UTS), MPa 430 to 550
450 to 520
Tensile Strength: Yield (Proof), MPa 420 to 550
410 to 480

Thermal Properties

Latent Heat of Fusion, J/g 210
200
Maximum Temperature: Mechanical, °C 200
180
Melting Completion (Liquidus), °C 1070
1070
Melting Onset (Solidus), °C 1050
1030
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 260
150
Thermal Expansion, µm/m-K 18
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
35
Electrical Conductivity: Equal Weight (Specific), % IACS 62
36

Otherwise Unclassified Properties

Base Metal Price, % relative 30
29
Density, g/cm3 8.9
8.7
Embodied Carbon, kg CO2/kg material 2.8
2.7
Embodied Energy, MJ/kg 43
43
Embodied Water, L/kg 320
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 49 to 52
40 to 66
Resilience: Unit (Modulus of Resilience), kJ/m3 770 to 1320
760 to 1030
Stiffness to Weight: Axial, points 7.2
7.2
Stiffness to Weight: Bending, points 18
19
Strength to Weight: Axial, points 14 to 17
14 to 17
Strength to Weight: Bending, points 14 to 17
15 to 16
Thermal Diffusivity, mm2/s 75
45
Thermal Shock Resistance, points 15 to 20
16 to 18

Alloy Composition

Copper (Cu), % 95.7 to 99.47
86.6 to 91
Iron (Fe), % 0.020 to 0.5
0 to 0.050
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 0.1 to 1.0
0
Nickel (Ni), % 0
0.3 to 1.0
Phosphorus (P), % 0.010 to 0.1
0.050 to 0.2
Tin (Sn), % 0.1 to 1.0
0.2 to 0.7
Zinc (Zn), % 0.3 to 1.5
6.5 to 12.9
Residuals, % 0
0 to 0.5