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C66900 Brass vs. C71580 Copper-nickel

Both C66900 brass and C71580 copper-nickel 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 C66900 brass and the bottom bar is C71580 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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