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H04 C61500 Bronze vs. H04 C66900 Brass

Both H04 C61500 bronze and H04 C66900 brass are copper alloys. Both are furnished in the H04 (full hard) temper. They have 64% of their average alloy composition in common. There are 28 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 C61500 bronze and the bottom bar is H04 C66900 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 5.0
5.0
Poisson's Ratio 0.34
0.32
Rockwell Superficial 30T Hardness 83
77
Shear Modulus, GPa 42
45
Shear Strength, MPa 500
360
Tensile Strength: Ultimate (UTS), MPa 860
610
Tensile Strength: Yield (Proof), MPa 620
590

Thermal Properties

Latent Heat of Fusion, J/g 220
190
Maximum Temperature: Mechanical, °C 220
150
Melting Completion (Liquidus), °C 1040
860
Melting Onset (Solidus), °C 1030
850
Specific Heat Capacity, J/kg-K 430
400
Thermal Expansion, µm/m-K 18
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 13
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 13
3.8

Otherwise Unclassified Properties

Base Metal Price, % relative 29
23
Density, g/cm3 8.4
8.2
Embodied Carbon, kg CO2/kg material 3.2
2.8
Embodied Energy, MJ/kg 52
46
Embodied Water, L/kg 380
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 39
30
Resilience: Unit (Modulus of Resilience), kJ/m3 1700
1480
Stiffness to Weight: Axial, points 7.5
8.1
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 28
21
Strength to Weight: Bending, points 24
20
Thermal Shock Resistance, points 31
18

Alloy Composition


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Aluminum (Al), % 7.7 to 8.3
0
Copper (Cu), % 89 to 90.5
62.5 to 64.5
Iron (Fe), % 0
0 to 0.25
Lead (Pb), % 0 to 0.015
0 to 0.050
Manganese (Mn), % 0
11.5 to 12.5
Nickel (Ni), % 1.8 to 2.2
0
Zinc (Zn), % 0
22.5 to 26
Residuals, % 0 to 0.5
0 to 0.2