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C26200 Brass vs. C71580 Copper-nickel

Both C26200 brass and C71580 copper-nickel are copper alloys. They have 68% of their average alloy composition in common. There are 29 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 C26200 brass and the bottom bar is C71580 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
140
Elongation at Break, % 3.0 to 180
40
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 41
51
Shear Strength, MPa 230 to 390
230
Tensile Strength: Ultimate (UTS), MPa 330 to 770
330
Tensile Strength: Yield (Proof), MPa 110 to 490
110

Thermal Properties

Latent Heat of Fusion, J/g 180
230
Maximum Temperature: Mechanical, °C 140
260
Melting Completion (Liquidus), °C 950
1180
Melting Onset (Solidus), °C 920
1120
Specific Heat Capacity, J/kg-K 390
400
Thermal Conductivity, W/m-K 120
39
Thermal Expansion, µm/m-K 20
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
4.7
Electrical Conductivity: Equal Weight (Specific), % IACS 31
4.7

Otherwise Unclassified Properties

Base Metal Price, % relative 25
41
Density, g/cm3 8.2
8.9
Embodied Carbon, kg CO2/kg material 2.7
5.1
Embodied Energy, MJ/kg 45
74
Embodied Water, L/kg 320
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 160
100
Resilience: Unit (Modulus of Resilience), kJ/m3 62 to 1110
47
Stiffness to Weight: Axial, points 7.2
8.5
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 11 to 26
10
Strength to Weight: Bending, points 13 to 23
12
Thermal Diffusivity, mm2/s 38
11
Thermal Shock Resistance, points 11 to 26
11

Alloy Composition

Carbon (C), % 0
0 to 0.070
Copper (Cu), % 67 to 70
65.5 to 71
Iron (Fe), % 0 to 0.050
0 to 0.5
Lead (Pb), % 0 to 0.070
0 to 0.050
Manganese (Mn), % 0
0 to 0.3
Nickel (Ni), % 0
29 to 33
Zinc (Zn), % 29.6 to 33
0 to 0.050
Residuals, % 0
0 to 0.5