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C66200 Brass vs. CR018A Copper

Both C66200 brass and CR018A 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 (1, in this case) are not shown.

For each property being compared, the top bar is C66200 brass and the bottom bar is CR018A copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 8.0 to 15
15
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 42
43
Tensile Strength: Ultimate (UTS), MPa 450 to 520
220
Tensile Strength: Yield (Proof), MPa 410 to 480
130

Thermal Properties

Latent Heat of Fusion, J/g 200
210
Maximum Temperature: Mechanical, °C 180
200
Melting Completion (Liquidus), °C 1070
1090
Melting Onset (Solidus), °C 1030
1040
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 150
390
Thermal Expansion, µm/m-K 18
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
100
Electrical Conductivity: Equal Weight (Specific), % IACS 36
100

Otherwise Unclassified Properties

Base Metal Price, % relative 29
33
Density, g/cm3 8.7
9.0
Embodied Carbon, kg CO2/kg material 2.7
2.7
Embodied Energy, MJ/kg 43
42
Embodied Water, L/kg 320
360

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
29
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
76
Stiffness to Weight: Axial, points 7.2
7.2
Stiffness to Weight: Bending, points 19
18
Strength to Weight: Axial, points 14 to 17
6.8
Strength to Weight: Bending, points 15 to 16
9.0
Thermal Diffusivity, mm2/s 45
110
Thermal Shock Resistance, points 16 to 18
7.8

Alloy Composition

Bismuth (Bi), % 0
0 to 0.00050
Copper (Cu), % 86.6 to 91
99.914 to 99.94
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
Silver (Ag), % 0
0.060 to 0.080
Tin (Sn), % 0.2 to 0.7
0
Zinc (Zn), % 6.5 to 12.9
0
Residuals, % 0 to 0.5
0