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C63200 Bronze vs. C85700 Brass

Both C63200 bronze and C85700 brass are copper alloys. They have 63% 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 C63200 bronze and the bottom bar is C85700 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
100
Elongation at Break, % 17 to 18
17
Poisson's Ratio 0.34
0.31
Shear Modulus, GPa 44
40
Tensile Strength: Ultimate (UTS), MPa 640 to 710
310
Tensile Strength: Yield (Proof), MPa 310 to 350
110

Thermal Properties

Latent Heat of Fusion, J/g 230
170
Maximum Temperature: Mechanical, °C 230
120
Melting Completion (Liquidus), °C 1060
940
Melting Onset (Solidus), °C 1040
910
Specific Heat Capacity, J/kg-K 440
380
Thermal Conductivity, W/m-K 35
84
Thermal Expansion, µm/m-K 18
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
22
Electrical Conductivity: Equal Weight (Specific), % IACS 7.6
25

Otherwise Unclassified Properties

Base Metal Price, % relative 29
24
Density, g/cm3 8.3
8.0
Embodied Carbon, kg CO2/kg material 3.4
2.8
Embodied Energy, MJ/kg 55
47
Embodied Water, L/kg 380
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 95 to 99
41
Resilience: Unit (Modulus of Resilience), kJ/m3 400 to 510
59
Stiffness to Weight: Axial, points 7.9
7.2
Stiffness to Weight: Bending, points 20
20
Strength to Weight: Axial, points 21 to 24
11
Strength to Weight: Bending, points 20 to 21
13
Thermal Diffusivity, mm2/s 9.6
27
Thermal Shock Resistance, points 22 to 24
10

Alloy Composition

Aluminum (Al), % 8.7 to 9.5
0 to 0.8
Copper (Cu), % 78.8 to 82.6
58 to 64
Iron (Fe), % 3.5 to 4.3
0 to 0.7
Lead (Pb), % 0 to 0.020
0.8 to 1.5
Manganese (Mn), % 1.2 to 2.0
0
Nickel (Ni), % 4.0 to 4.8
0 to 1.0
Silicon (Si), % 0 to 0.1
0 to 0.050
Tin (Sn), % 0
0.5 to 1.5
Zinc (Zn), % 0
32 to 40
Residuals, % 0
0 to 1.3