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CC767S Brass vs. C33200 Brass

Both CC767S brass and C33200 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 CC767S brass and the bottom bar is C33200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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