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C66700 Brass vs. C81500 Copper

Both C66700 brass and C81500 copper are copper alloys. They have 70% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is C66700 brass and the bottom bar is C81500 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 2.0 to 58
17
Poisson's Ratio 0.31
0.34
Shear Modulus, GPa 41
44
Tensile Strength: Ultimate (UTS), MPa 340 to 690
350
Tensile Strength: Yield (Proof), MPa 100 to 640
280

Thermal Properties

Latent Heat of Fusion, J/g 180
210
Maximum Temperature: Mechanical, °C 140
200
Melting Completion (Liquidus), °C 1090
1090
Melting Onset (Solidus), °C 1050
1080
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 97
320
Thermal Expansion, µm/m-K 20
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 17
82
Electrical Conductivity: Equal Weight (Specific), % IACS 19
83

Otherwise Unclassified Properties

Base Metal Price, % relative 25
31
Density, g/cm3 8.2
8.9
Embodied Carbon, kg CO2/kg material 2.7
2.6
Embodied Energy, MJ/kg 45
41
Embodied Water, L/kg 320
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 150
56
Resilience: Unit (Modulus of Resilience), kJ/m3 49 to 1900
330
Stiffness to Weight: Axial, points 7.3
7.3
Stiffness to Weight: Bending, points 19
18
Strength to Weight: Axial, points 11 to 23
11
Strength to Weight: Bending, points 13 to 21
12
Thermal Diffusivity, mm2/s 30
91
Thermal Shock Resistance, points 11 to 23
12

Alloy Composition

Aluminum (Al), % 0
0 to 0.1
Chromium (Cr), % 0
0.4 to 1.5
Copper (Cu), % 68.5 to 71.5
97.4 to 99.6
Iron (Fe), % 0 to 0.1
0 to 0.1
Lead (Pb), % 0 to 0.070
0 to 0.020
Manganese (Mn), % 0.8 to 1.5
0
Silicon (Si), % 0
0 to 0.15
Tin (Sn), % 0
0 to 0.1
Zinc (Zn), % 26.3 to 30.7
0 to 0.1
Residuals, % 0
0 to 0.5