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C33200 Brass vs. CC767S Brass

Both C33200 brass and CC767S brass are copper alloys. They have a moderately high 92% 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 C33200 brass and the bottom bar is CC767S brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
110
Elongation at Break, % 7.0 to 60
34
Poisson's Ratio 0.31
0.31
Shear Modulus, GPa 40
40
Tensile Strength: Ultimate (UTS), MPa 320 to 520
430
Tensile Strength: Yield (Proof), MPa 110 to 450
150

Thermal Properties

Latent Heat of Fusion, J/g 170
180
Maximum Temperature: Mechanical, °C 130
120
Melting Completion (Liquidus), °C 930
840
Melting Onset (Solidus), °C 900
790
Specific Heat Capacity, J/kg-K 380
390
Thermal Conductivity, W/m-K 120
110
Thermal Expansion, µm/m-K 20
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
32
Electrical Conductivity: Equal Weight (Specific), % IACS 28
36

Otherwise Unclassified Properties

Base Metal Price, % relative 24
23
Density, g/cm3 8.2
8.0
Embodied Carbon, kg CO2/kg material 2.6
2.7
Embodied Energy, MJ/kg 44
47
Embodied Water, L/kg 320
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 35 to 150
110
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 960
100
Stiffness to Weight: Axial, points 7.1
7.3
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 11 to 17
15
Strength to Weight: Bending, points 13 to 17
16
Thermal Diffusivity, mm2/s 37
34
Thermal Shock Resistance, points 11 to 17
14

Alloy Composition


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Aluminum (Al), % 0
0.1 to 0.8
Copper (Cu), % 65 to 68
58 to 64
Iron (Fe), % 0 to 0.070
0 to 0.5
Lead (Pb), % 1.5 to 2.5
0 to 0.1
Manganese (Mn), % 0
0 to 0.5
Nickel (Ni), % 0
0 to 1.0
Silicon (Si), % 0
0 to 0.2
Tin (Sn), % 0
0 to 0.1
Zinc (Zn), % 29 to 33.5
32.8 to 41.9
Residuals, % 0 to 0.4
0