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H01 C21000 Brass vs. H01 C71520 Copper-nickel

Both H01 C21000 brass and H01 C71520 copper-nickel are copper alloys. Both are furnished in the H01 (quarter hard) temper. They have 69% of their average alloy composition in common.

For each property being compared, the top bar is H01 C21000 brass and the bottom bar is H01 C71520 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
140
Elongation at Break, % 29
17
Poisson's Ratio 0.34
0.33
Rockwell B Hardness 36
74
Rockwell Superficial 30T Hardness 44
66
Shear Modulus, GPa 43
51
Shear Strength, MPa 190
280
Tensile Strength: Ultimate (UTS), MPa 290
460
Tensile Strength: Yield (Proof), MPa 230
340

Thermal Properties

Latent Heat of Fusion, J/g 200
230
Maximum Temperature: Mechanical, °C 190
260
Melting Completion (Liquidus), °C 1070
1170
Melting Onset (Solidus), °C 1050
1120
Specific Heat Capacity, J/kg-K 390
400
Thermal Conductivity, W/m-K 230
32
Thermal Expansion, µm/m-K 18
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 56
5.7
Electrical Conductivity: Equal Weight (Specific), % IACS 57
5.8

Otherwise Unclassified Properties

Base Metal Price, % relative 30
40
Density, g/cm3 8.8
8.9
Embodied Carbon, kg CO2/kg material 2.6
5.0
Embodied Energy, MJ/kg 42
73
Embodied Water, L/kg 310
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 80
71
Resilience: Unit (Modulus of Resilience), kJ/m3 240
420
Stiffness to Weight: Axial, points 7.2
8.6
Stiffness to Weight: Bending, points 18
19
Strength to Weight: Axial, points 9.1
14
Strength to Weight: Bending, points 11
15
Thermal Diffusivity, mm2/s 69
8.9
Thermal Shock Resistance, points 10
16

Alloy Composition

Carbon (C), % 0
0 to 0.050
Copper (Cu), % 94 to 96
65 to 71.6
Iron (Fe), % 0 to 0.050
0.4 to 1.0
Lead (Pb), % 0 to 0.030
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), % 3.7 to 6.0
0 to 0.5
Residuals, % 0
0 to 0.5