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H04 C66900 Brass vs. H04 C71500 Copper-nickel

Both H04 C66900 brass and H04 C71500 copper-nickel are copper alloys. Both are furnished in the H04 (full hard) temper. They have 65% 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 H04 C66900 brass and the bottom bar is H04 C71500 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
140
Elongation at Break, % 5.0
10
Poisson's Ratio 0.32
0.33
Rockwell B Hardness 88
86
Rockwell Superficial 30T Hardness 77
74
Shear Modulus, GPa 45
52
Shear Strength, MPa 360
340
Tensile Strength: Ultimate (UTS), MPa 610
570
Tensile Strength: Yield (Proof), MPa 590
430

Thermal Properties

Latent Heat of Fusion, J/g 190
230
Maximum Temperature: Mechanical, °C 150
260
Melting Completion (Liquidus), °C 860
1240
Melting Onset (Solidus), °C 850
1170
Specific Heat Capacity, J/kg-K 400
400
Thermal Expansion, µm/m-K 20
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
4.6
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 30
54
Resilience: Unit (Modulus of Resilience), kJ/m3 1480
680
Stiffness to Weight: Axial, points 8.1
8.6
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 21
18
Strength to Weight: Bending, points 20
17
Thermal Shock Resistance, points 18
18

Alloy Composition


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Copper (Cu), % 62.5 to 64.5
63.5 to 70.6
Iron (Fe), % 0 to 0.25
0.4 to 1.0
Lead (Pb), % 0 to 0.050
0 to 0.050
Manganese (Mn), % 11.5 to 12.5
0 to 1.0
Nickel (Ni), % 0
29 to 33
Zinc (Zn), % 22.5 to 26
0 to 1.0
Residuals, % 0 to 0.2
0 to 0.5