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H02 C26200 Brass vs. H02 C65400 Bronze

Both H02 C26200 brass and H02 C65400 bronze are copper alloys. Both are furnished in the H02 (half hard) temper. They have 69% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is H02 C26200 brass and the bottom bar is H02 C65400 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 180
20
Poisson's Ratio 0.31
0.34
Rockwell B Hardness 75
92
Rockwell Superficial 30T Hardness 65
77
Shear Modulus, GPa 41
43
Shear Strength, MPa 280
400
Tensile Strength: Ultimate (UTS), MPa 460
650
Tensile Strength: Yield (Proof), MPa 390
370

Thermal Properties

Latent Heat of Fusion, J/g 180
260
Maximum Temperature: Mechanical, °C 140
200
Melting Completion (Liquidus), °C 950
1020
Melting Onset (Solidus), °C 920
960
Specific Heat Capacity, J/kg-K 390
400
Thermal Conductivity, W/m-K 120
36
Thermal Expansion, µm/m-K 20
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
7.0
Electrical Conductivity: Equal Weight (Specific), % IACS 31
7.3

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Unit (Modulus of Resilience), kJ/m3 710
600
Stiffness to Weight: Axial, points 7.2
7.3
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 15
21
Strength to Weight: Bending, points 16
19
Thermal Diffusivity, mm2/s 38
10
Thermal Shock Resistance, points 15
24

Alloy Composition

Chromium (Cr), % 0
0.010 to 0.12
Copper (Cu), % 67 to 70
93.8 to 96.1
Iron (Fe), % 0 to 0.050
0
Lead (Pb), % 0 to 0.070
0 to 0.050
Silicon (Si), % 0
2.7 to 3.4
Tin (Sn), % 0
1.2 to 1.9
Zinc (Zn), % 29.6 to 33
0 to 0.5
Residuals, % 0
0 to 0.2