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C66200 Brass vs. C19800 Copper

Both C66200 brass and C19800 copper 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 C66200 brass and the bottom bar is C19800 copper.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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