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H01 C35600 Brass vs. H01 C71520 Copper-nickel

Both H01 C35600 brass and H01 C71520 copper-nickel are copper alloys. Both are furnished in the H01 (quarter hard) temper. They have 62% of their average alloy composition in common.

For each property being compared, the top bar is H01 C35600 brass and the bottom bar is H01 C71520 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
140
Elongation at Break, % 17
17
Poisson's Ratio 0.31
0.33
Rockwell B Hardness 53
74
Rockwell Superficial 30T Hardness 52
66
Shear Modulus, GPa 39
51
Shear Strength, MPa 230
280
Tensile Strength: Ultimate (UTS), MPa 380
460
Tensile Strength: Yield (Proof), MPa 160
340

Thermal Properties

Latent Heat of Fusion, J/g 170
230
Maximum Temperature: Mechanical, °C 120
260
Melting Completion (Liquidus), °C 900
1170
Melting Onset (Solidus), °C 890
1120
Specific Heat Capacity, J/kg-K 380
400
Thermal Conductivity, W/m-K 120
32
Thermal Expansion, µm/m-K 21
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
5.7
Electrical Conductivity: Equal Weight (Specific), % IACS 29
5.8

Otherwise Unclassified Properties

Base Metal Price, % relative 23
40
Density, g/cm3 8.1
8.9
Embodied Carbon, kg CO2/kg material 2.6
5.0
Embodied Energy, MJ/kg 45
73
Embodied Water, L/kg 320
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 52
71
Resilience: Unit (Modulus of Resilience), kJ/m3 120
420
Stiffness to Weight: Axial, points 7.0
8.6
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 13
14
Strength to Weight: Bending, points 14
15
Thermal Diffusivity, mm2/s 38
8.9
Thermal Shock Resistance, points 13
16

Alloy Composition


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Carbon (C), % 0
0 to 0.050
Copper (Cu), % 60 to 63
65 to 71.6
Iron (Fe), % 0 to 0.1
0.4 to 1.0
Lead (Pb), % 2.0 to 3.0
0 to 0.020
Manganese (Mn), % 0
0 to 1.0
Nickel (Ni), % 0
28 to 33
Phosphorus (P), % 0
0 to 0.2
Sulfur (S), % 0
0 to 0.020
Zinc (Zn), % 33.4 to 38
0 to 0.5
Residuals, % 0 to 0.5
0 to 0.5