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C66700 Brass vs. C86500 Bronze

Both C66700 brass and C86500 bronze are copper alloys. They have 87% 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 C66700 brass and the bottom bar is C86500 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 2.0 to 58
25
Poisson's Ratio 0.31
0.3
Shear Modulus, GPa 41
40
Tensile Strength: Ultimate (UTS), MPa 340 to 690
530
Tensile Strength: Yield (Proof), MPa 100 to 640
190

Thermal Properties

Latent Heat of Fusion, J/g 180
170
Maximum Temperature: Mechanical, °C 140
120
Melting Completion (Liquidus), °C 1090
880
Melting Onset (Solidus), °C 1050
860
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 97
86
Thermal Expansion, µm/m-K 20
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 17
22
Electrical Conductivity: Equal Weight (Specific), % IACS 19
25

Otherwise Unclassified Properties

Base Metal Price, % relative 25
23
Density, g/cm3 8.2
7.9
Embodied Carbon, kg CO2/kg material 2.7
2.8
Embodied Energy, MJ/kg 45
48
Embodied Water, L/kg 320
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 150
110
Resilience: Unit (Modulus of Resilience), kJ/m3 49 to 1900
180
Stiffness to Weight: Axial, points 7.3
7.4
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 11 to 23
19
Strength to Weight: Bending, points 13 to 21
18
Thermal Diffusivity, mm2/s 30
28
Thermal Shock Resistance, points 11 to 23
17

Alloy Composition

Aluminum (Al), % 0
0.5 to 1.5
Copper (Cu), % 68.5 to 71.5
55 to 60
Iron (Fe), % 0 to 0.1
0.4 to 2.0
Lead (Pb), % 0 to 0.070
0 to 0.4
Manganese (Mn), % 0.8 to 1.5
0.1 to 1.5
Nickel (Ni), % 0
0 to 1.0
Tin (Sn), % 0
0 to 1.0
Zinc (Zn), % 26.3 to 30.7
36 to 42
Residuals, % 0
0 to 1.0