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CC767S Brass vs. C61900 Bronze

Both CC767S brass and C61900 bronze are copper alloys. They have 62% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is CC767S brass and the bottom bar is C61900 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 34
21 to 32
Poisson's Ratio 0.31
0.34
Shear Modulus, GPa 40
43
Tensile Strength: Ultimate (UTS), MPa 430
570 to 650
Tensile Strength: Yield (Proof), MPa 150
230 to 310

Thermal Properties

Latent Heat of Fusion, J/g 180
230
Maximum Temperature: Mechanical, °C 120
220
Melting Completion (Liquidus), °C 840
1050
Melting Onset (Solidus), °C 790
1040
Specific Heat Capacity, J/kg-K 390
440
Thermal Conductivity, W/m-K 110
79
Thermal Expansion, µm/m-K 21
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
11
Electrical Conductivity: Equal Weight (Specific), % IACS 36
11

Otherwise Unclassified Properties

Base Metal Price, % relative 23
28
Density, g/cm3 8.0
8.3
Embodied Carbon, kg CO2/kg material 2.7
3.1
Embodied Energy, MJ/kg 47
51
Embodied Water, L/kg 330
380

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 100
230 to 430
Stiffness to Weight: Axial, points 7.3
7.6
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 15
19 to 22
Strength to Weight: Bending, points 16
18 to 20
Thermal Diffusivity, mm2/s 34
22
Thermal Shock Resistance, points 14
20 to 23

Alloy Composition


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Aluminum (Al), % 0.1 to 0.8
8.5 to 10
Copper (Cu), % 58 to 64
83.6 to 88.5
Iron (Fe), % 0 to 0.5
3.0 to 4.5
Lead (Pb), % 0 to 0.1
0 to 0.020
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 to 0.6
Zinc (Zn), % 32.8 to 41.9
0 to 0.8
Residuals, % 0
0 to 0.5