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H01 C65400 Bronze vs. H01 C66700 Brass

Both H01 C65400 bronze and H01 C66700 brass are copper alloys. Both are furnished in the H01 (quarter hard) temper. They have 70% of their average alloy composition in common.

For each property being compared, the top bar is H01 C65400 bronze and the bottom bar is H01 C66700 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 28
38
Poisson's Ratio 0.34
0.31
Rockwell B Hardness 82
57
Rockwell Superficial 30T Hardness 71
55
Shear Modulus, GPa 43
41
Shear Strength, MPa 370
260
Tensile Strength: Ultimate (UTS), MPa 570
390
Tensile Strength: Yield (Proof), MPa 270
260

Thermal Properties

Latent Heat of Fusion, J/g 260
180
Maximum Temperature: Mechanical, °C 200
140
Melting Completion (Liquidus), °C 1020
1090
Melting Onset (Solidus), °C 960
1050
Specific Heat Capacity, J/kg-K 400
390
Thermal Conductivity, W/m-K 36
97
Thermal Expansion, µm/m-K 17
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
17
Electrical Conductivity: Equal Weight (Specific), % IACS 7.3
19

Otherwise Unclassified Properties

Base Metal Price, % relative 31
25
Density, g/cm3 8.7
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.7
Embodied Energy, MJ/kg 45
45
Embodied Water, L/kg 310
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130
130
Resilience: Unit (Modulus of Resilience), kJ/m3 320
310
Stiffness to Weight: Axial, points 7.3
7.3
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 18
13
Strength to Weight: Bending, points 18
14
Thermal Diffusivity, mm2/s 10
30
Thermal Shock Resistance, points 21
13

Alloy Composition

Chromium (Cr), % 0.010 to 0.12
0
Copper (Cu), % 93.8 to 96.1
68.5 to 71.5
Iron (Fe), % 0
0 to 0.1
Lead (Pb), % 0 to 0.050
0 to 0.070
Manganese (Mn), % 0
0.8 to 1.5
Silicon (Si), % 2.7 to 3.4
0
Tin (Sn), % 1.2 to 1.9
0
Zinc (Zn), % 0 to 0.5
26.3 to 30.7
Residuals, % 0
0 to 0.5