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C85500 Brass vs. C66200 Brass

Both C85500 brass and C66200 brass are copper alloys. They have 71% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.

For each property being compared, the top bar is C85500 brass and the bottom bar is C66200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
110
Elongation at Break, % 40
8.0 to 15
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 40
42
Tensile Strength: Ultimate (UTS), MPa 410
450 to 520
Tensile Strength: Yield (Proof), MPa 160
410 to 480

Thermal Properties

Latent Heat of Fusion, J/g 170
200
Maximum Temperature: Mechanical, °C 120
180
Melting Completion (Liquidus), °C 900
1070
Melting Onset (Solidus), °C 890
1030
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 120
150
Thermal Expansion, µm/m-K 21
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
35
Electrical Conductivity: Equal Weight (Specific), % IACS 29
36

Otherwise Unclassified Properties

Base Metal Price, % relative 23
29
Density, g/cm3 8.0
8.7
Embodied Carbon, kg CO2/kg material 2.7
2.7
Embodied Energy, MJ/kg 46
43
Embodied Water, L/kg 320
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130
40 to 66
Resilience: Unit (Modulus of Resilience), kJ/m3 120
760 to 1030
Stiffness to Weight: Axial, points 7.3
7.2
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 14
14 to 17
Strength to Weight: Bending, points 15
15 to 16
Thermal Diffusivity, mm2/s 38
45
Thermal Shock Resistance, points 14
16 to 18

Alloy Composition


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Copper (Cu), % 59 to 63
86.6 to 91
Iron (Fe), % 0 to 0.2
0 to 0.050
Lead (Pb), % 0 to 0.2
0 to 0.050
Manganese (Mn), % 0 to 0.2
0
Nickel (Ni), % 0 to 0.2
0.3 to 1.0
Phosphorus (P), % 0
0.050 to 0.2
Tin (Sn), % 0 to 0.2
0.2 to 0.7
Zinc (Zn), % 35.1 to 41
6.5 to 12.9
Residuals, % 0 to 0.9
0 to 0.5