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H04 C26200 Brass vs. H04 C61500 Bronze

Both H04 C26200 brass and H04 C61500 bronze are copper alloys. Both are furnished in the H04 (full 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 H04 C26200 brass and the bottom bar is H04 C61500 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 8.0
5.0
Poisson's Ratio 0.31
0.34
Rockwell Superficial 30T Hardness 73
83
Shear Modulus, GPa 41
42
Shear Strength, MPa 300
500
Tensile Strength: Ultimate (UTS), MPa 530
860
Tensile Strength: Yield (Proof), MPa 480
620

Thermal Properties

Latent Heat of Fusion, J/g 180
220
Maximum Temperature: Mechanical, °C 140
220
Melting Completion (Liquidus), °C 950
1040
Melting Onset (Solidus), °C 920
1030
Specific Heat Capacity, J/kg-K 390
430
Thermal Conductivity, W/m-K 120
58
Thermal Expansion, µm/m-K 20
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
13
Electrical Conductivity: Equal Weight (Specific), % IACS 31
13

Otherwise Unclassified Properties

Base Metal Price, % relative 25
29
Density, g/cm3 8.2
8.4
Embodied Carbon, kg CO2/kg material 2.7
3.2
Embodied Energy, MJ/kg 45
52
Embodied Water, L/kg 320
380

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 41
39
Resilience: Unit (Modulus of Resilience), kJ/m3 1060
1700
Stiffness to Weight: Axial, points 7.2
7.5
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 18
28
Strength to Weight: Bending, points 18
24
Thermal Diffusivity, mm2/s 38
16
Thermal Shock Resistance, points 18
31

Alloy Composition

Aluminum (Al), % 0
7.7 to 8.3
Copper (Cu), % 67 to 70
89 to 90.5
Iron (Fe), % 0 to 0.050
0
Lead (Pb), % 0 to 0.070
0 to 0.015
Nickel (Ni), % 0
1.8 to 2.2
Zinc (Zn), % 29.6 to 33
0
Residuals, % 0
0 to 0.5