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H06 C65400 Bronze vs. H06 C68800 Brass

Both H06 C65400 bronze and H06 C68800 brass are copper alloys. Both are furnished in the H06 (extra hard) temper. They have 74% of their average alloy composition in common.

For each property being compared, the top bar is H06 C65400 bronze and the bottom bar is H06 C68800 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 7.8
3.0
Poisson's Ratio 0.34
0.32
Rockwell B Hardness 99
97
Rockwell Superficial 30T Hardness 82
83
Shear Modulus, GPa 43
41
Shear Strength, MPa 490
460
Tensile Strength: Ultimate (UTS), MPa 840
810
Tensile Strength: Yield (Proof), MPa 530
720

Thermal Properties

Latent Heat of Fusion, J/g 260
190
Maximum Temperature: Mechanical, °C 200
160
Melting Completion (Liquidus), °C 1020
960
Melting Onset (Solidus), °C 960
950
Specific Heat Capacity, J/kg-K 400
400
Thermal Conductivity, W/m-K 36
40
Thermal Expansion, µm/m-K 17
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
18
Electrical Conductivity: Equal Weight (Specific), % IACS 7.3
20

Otherwise Unclassified Properties

Base Metal Price, % relative 31
26
Density, g/cm3 8.7
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.8
Embodied Energy, MJ/kg 45
48
Embodied Water, L/kg 310
350

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 57
23
Resilience: Unit (Modulus of Resilience), kJ/m3 1220
2430
Stiffness to Weight: Axial, points 7.3
7.3
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 27
27
Strength to Weight: Bending, points 23
24
Thermal Diffusivity, mm2/s 10
12
Thermal Shock Resistance, points 31
27

Alloy Composition


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Aluminum (Al), % 0
3.0 to 3.8
Chromium (Cr), % 0.010 to 0.12
0
Cobalt (Co), % 0
0.25 to 0.55
Copper (Cu), % 93.8 to 96.1
70.8 to 75.5
Iron (Fe), % 0
0 to 0.2
Lead (Pb), % 0 to 0.050
0 to 0.050
Silicon (Si), % 2.7 to 3.4
0
Tin (Sn), % 1.2 to 1.9
0
Zinc (Zn), % 0 to 0.5
21.3 to 24.1
Residuals, % 0 to 0.2
0 to 0.5