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C26200 Brass vs. C86500 Bronze

Both C26200 brass and C86500 bronze 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 C26200 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, % 3.0 to 180
25
Poisson's Ratio 0.31
0.3
Shear Modulus, GPa 41
40
Tensile Strength: Ultimate (UTS), MPa 330 to 770
530
Tensile Strength: Yield (Proof), MPa 110 to 490
190

Thermal Properties

Latent Heat of Fusion, J/g 180
170
Maximum Temperature: Mechanical, °C 140
120
Melting Completion (Liquidus), °C 950
880
Melting Onset (Solidus), °C 920
860
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 120
86
Thermal Expansion, µm/m-K 20
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
22
Electrical Conductivity: Equal Weight (Specific), % IACS 31
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 19 to 160
110
Resilience: Unit (Modulus of Resilience), kJ/m3 62 to 1110
180
Stiffness to Weight: Axial, points 7.2
7.4
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 11 to 26
19
Strength to Weight: Bending, points 13 to 23
18
Thermal Diffusivity, mm2/s 38
28
Thermal Shock Resistance, points 11 to 26
17

Alloy Composition


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Aluminum (Al), % 0
0.5 to 1.5
Copper (Cu), % 67 to 70
55 to 60
Iron (Fe), % 0 to 0.050
0.4 to 2.0
Lead (Pb), % 0 to 0.070
0 to 0.4
Manganese (Mn), % 0
0.1 to 1.5
Nickel (Ni), % 0
0 to 1.0
Tin (Sn), % 0
0 to 1.0
Zinc (Zn), % 29.6 to 33
36 to 42
Residuals, % 0 to 0.3
0 to 1.0