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CR011A Copper vs. C61400 Bronze

Both CR011A copper and C61400 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 (1, in this case) are not shown.

For each property being compared, the top bar is CR011A copper and the bottom bar is C61400 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 15
34 to 40
Poisson's Ratio 0.34
0.34
Shear Modulus, GPa 43
43
Tensile Strength: Ultimate (UTS), MPa 220
540 to 570
Tensile Strength: Yield (Proof), MPa 130
220 to 270

Thermal Properties

Latent Heat of Fusion, J/g 210
220
Maximum Temperature: Mechanical, °C 200
220
Melting Completion (Liquidus), °C 1090
1050
Melting Onset (Solidus), °C 1040
1040
Specific Heat Capacity, J/kg-K 390
420
Thermal Conductivity, W/m-K 390
67
Thermal Expansion, µm/m-K 17
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 100
14
Electrical Conductivity: Equal Weight (Specific), % IACS 100
15

Otherwise Unclassified Properties

Base Metal Price, % relative 32
28
Density, g/cm3 9.0
8.5
Embodied Carbon, kg CO2/kg material 2.6
3.0
Embodied Energy, MJ/kg 42
48
Embodied Water, L/kg 340
360

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29
160 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 76
210 to 310
Stiffness to Weight: Axial, points 7.2
7.5
Stiffness to Weight: Bending, points 18
19
Strength to Weight: Axial, points 6.8
18 to 19
Strength to Weight: Bending, points 9.0
17 to 18
Thermal Diffusivity, mm2/s 110
19
Thermal Shock Resistance, points 7.8
18 to 20

Alloy Composition

Aluminum (Al), % 0
6.0 to 8.0
Bismuth (Bi), % 0 to 0.00050
0
Copper (Cu), % 99.88 to 99.97
86 to 92.5
Iron (Fe), % 0
1.5 to 3.5
Lead (Pb), % 0
0 to 0.010
Manganese (Mn), % 0
0 to 1.0
Oxygen (O), % 0 to 0.040
0
Phosphorus (P), % 0
0 to 0.015
Silver (Ag), % 0.030 to 0.050
0
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5