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C71580 Copper-nickel vs. C66900 Brass

Both C71580 copper-nickel and C66900 brass are copper alloys. They have 64% of their average alloy composition in common. There are 27 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is C71580 copper-nickel and the bottom bar is C66900 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
120
Elongation at Break, % 40
1.1 to 26
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 51
45
Shear Strength, MPa 230
290 to 440
Tensile Strength: Ultimate (UTS), MPa 330
460 to 770
Tensile Strength: Yield (Proof), MPa 110
330 to 760

Thermal Properties

Latent Heat of Fusion, J/g 230
190
Maximum Temperature: Mechanical, °C 260
150
Melting Completion (Liquidus), °C 1180
860
Melting Onset (Solidus), °C 1120
850
Specific Heat Capacity, J/kg-K 400
400
Thermal Expansion, µm/m-K 15
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.7
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 4.7
3.8

Otherwise Unclassified Properties

Base Metal Price, % relative 41
23
Density, g/cm3 8.9
8.2
Embodied Carbon, kg CO2/kg material 5.1
2.8
Embodied Energy, MJ/kg 74
46
Embodied Water, L/kg 280
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 100
4.6 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 47
460 to 2450
Stiffness to Weight: Axial, points 8.5
8.1
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 10
15 to 26
Strength to Weight: Bending, points 12
16 to 23
Thermal Shock Resistance, points 11
14 to 23

Alloy Composition

Carbon (C), % 0 to 0.070
0
Copper (Cu), % 65.5 to 71
62.5 to 64.5
Iron (Fe), % 0 to 0.5
0 to 0.25
Lead (Pb), % 0 to 0.050
0 to 0.050
Manganese (Mn), % 0 to 0.3
11.5 to 12.5
Nickel (Ni), % 29 to 33
0
Zinc (Zn), % 0 to 0.050
22.5 to 26
Residuals, % 0
0 to 0.2