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C66900 Brass vs. C18200 Copper

Both C66900 brass and C18200 copper are copper alloys. They have 64% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.

For each property being compared, the top bar is C66900 brass and the bottom bar is C18200 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
120
Elongation at Break, % 1.1 to 26
11 to 40
Poisson's Ratio 0.32
0.34
Rockwell B Hardness 65 to 100
65 to 82
Shear Modulus, GPa 45
44
Shear Strength, MPa 290 to 440
210 to 320
Tensile Strength: Ultimate (UTS), MPa 460 to 770
310 to 530
Tensile Strength: Yield (Proof), MPa 330 to 760
97 to 450

Thermal Properties

Latent Heat of Fusion, J/g 190
210
Maximum Temperature: Mechanical, °C 150
200
Melting Completion (Liquidus), °C 860
1080
Melting Onset (Solidus), °C 850
1070
Specific Heat Capacity, J/kg-K 400
390
Thermal Expansion, µm/m-K 20
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
80
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
81

Otherwise Unclassified Properties

Base Metal Price, % relative 23
31
Density, g/cm3 8.2
8.9
Embodied Carbon, kg CO2/kg material 2.8
2.6
Embodied Energy, MJ/kg 46
41
Embodied Water, L/kg 310
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
43 to 96
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
40 to 860
Stiffness to Weight: Axial, points 8.1
7.3
Stiffness to Weight: Bending, points 20
18
Strength to Weight: Axial, points 15 to 26
9.6 to 16
Strength to Weight: Bending, points 16 to 23
11 to 16
Thermal Shock Resistance, points 14 to 23
11 to 18

Alloy Composition

Chromium (Cr), % 0
0.6 to 1.2
Copper (Cu), % 62.5 to 64.5
98.6 to 99.4
Iron (Fe), % 0 to 0.25
0 to 0.1
Lead (Pb), % 0 to 0.050
0 to 0.050
Manganese (Mn), % 11.5 to 12.5
0
Silicon (Si), % 0
0 to 0.1
Zinc (Zn), % 22.5 to 26
0
Residuals, % 0 to 0.2
0