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C27200 Brass vs. C86500 Bronze

Both C27200 brass and C86500 bronze are copper alloys. They have a moderately high 94% 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 C27200 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, % 10 to 50
25
Poisson's Ratio 0.31
0.3
Shear Modulus, GPa 40
40
Tensile Strength: Ultimate (UTS), MPa 370 to 590
530
Tensile Strength: Yield (Proof), MPa 150 to 410
190

Thermal Properties

Latent Heat of Fusion, J/g 170
170
Maximum Temperature: Mechanical, °C 130
120
Melting Completion (Liquidus), °C 920
880
Melting Onset (Solidus), °C 870
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 24
23
Density, g/cm3 8.1
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 30 to 270
110
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 810
180
Stiffness to Weight: Axial, points 7.2
7.4
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 13 to 20
19
Strength to Weight: Bending, points 14 to 19
18
Thermal Diffusivity, mm2/s 37
28
Thermal Shock Resistance, points 12 to 20
17

Alloy Composition

Aluminum (Al), % 0
0.5 to 1.5
Copper (Cu), % 62 to 65
55 to 60
Iron (Fe), % 0 to 0.070
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), % 34.6 to 38
36 to 42
Residuals, % 0
0 to 1.0