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C67000 Bronze vs. C85500 Brass

Both C67000 bronze and C85500 brass are copper alloys. They have 89% 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 C67000 bronze and the bottom bar is C85500 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
100
Elongation at Break, % 5.6 to 11
40
Poisson's Ratio 0.31
0.31
Shear Modulus, GPa 42
40
Tensile Strength: Ultimate (UTS), MPa 660 to 880
410
Tensile Strength: Yield (Proof), MPa 350 to 540
160

Thermal Properties

Latent Heat of Fusion, J/g 190
170
Maximum Temperature: Mechanical, °C 160
120
Melting Completion (Liquidus), °C 900
900
Melting Onset (Solidus), °C 850
890
Specific Heat Capacity, J/kg-K 410
390
Thermal Conductivity, W/m-K 99
120
Thermal Expansion, µm/m-K 20
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 22
26
Electrical Conductivity: Equal Weight (Specific), % IACS 25
29

Otherwise Unclassified Properties

Base Metal Price, % relative 23
23
Density, g/cm3 7.9
8.0
Embodied Carbon, kg CO2/kg material 2.9
2.7
Embodied Energy, MJ/kg 49
46
Embodied Water, L/kg 350
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 43 to 62
130
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 1290
120
Stiffness to Weight: Axial, points 7.8
7.3
Stiffness to Weight: Bending, points 20
20
Strength to Weight: Axial, points 23 to 31
14
Strength to Weight: Bending, points 21 to 26
15
Thermal Diffusivity, mm2/s 30
38
Thermal Shock Resistance, points 21 to 29
14

Alloy Composition


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Aluminum (Al), % 3.0 to 6.0
0
Copper (Cu), % 63 to 68
59 to 63
Iron (Fe), % 2.0 to 4.0
0 to 0.2
Lead (Pb), % 0 to 0.2
0 to 0.2
Manganese (Mn), % 2.5 to 5.0
0 to 0.2
Nickel (Ni), % 0
0 to 0.2
Tin (Sn), % 0 to 0.5
0 to 0.2
Zinc (Zn), % 21.8 to 32.5
35.1 to 41
Residuals, % 0 to 0.5
0 to 0.9