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C33200 Brass vs. C86200 Bronze

Both C33200 brass and C86200 bronze are copper alloys. They have 88% 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 C33200 brass and the bottom bar is C86200 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
110
Elongation at Break, % 7.0 to 60
21
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 40
42
Tensile Strength: Ultimate (UTS), MPa 320 to 520
710
Tensile Strength: Yield (Proof), MPa 110 to 450
350

Thermal Properties

Latent Heat of Fusion, J/g 170
190
Maximum Temperature: Mechanical, °C 130
160
Melting Completion (Liquidus), °C 930
940
Melting Onset (Solidus), °C 900
900
Specific Heat Capacity, J/kg-K 380
410
Thermal Conductivity, W/m-K 120
35
Thermal Expansion, µm/m-K 20
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
8.0
Electrical Conductivity: Equal Weight (Specific), % IACS 28
9.0

Otherwise Unclassified Properties

Base Metal Price, % relative 24
23
Density, g/cm3 8.2
8.0
Embodied Carbon, kg CO2/kg material 2.6
2.9
Embodied Energy, MJ/kg 44
49
Embodied Water, L/kg 320
340

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 35 to 150
120
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 960
540
Stiffness to Weight: Axial, points 7.1
7.8
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 11 to 17
25
Strength to Weight: Bending, points 13 to 17
22
Thermal Diffusivity, mm2/s 37
11
Thermal Shock Resistance, points 11 to 17
23

Alloy Composition

Aluminum (Al), % 0
3.0 to 4.9
Copper (Cu), % 65 to 68
60 to 66
Iron (Fe), % 0 to 0.070
2.0 to 4.0
Lead (Pb), % 1.5 to 2.5
0 to 0.2
Manganese (Mn), % 0
2.5 to 5.0
Nickel (Ni), % 0
0 to 1.0
Tin (Sn), % 0
0 to 0.2
Zinc (Zn), % 29 to 33.5
22 to 28
Residuals, % 0
0 to 1.0