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H10 C65400 Bronze vs. H10 C68800 Brass

Both H10 C65400 bronze and H10 C68800 brass are copper alloys. Both are furnished in the H10 (extra spring) temper. They have 74% of their average alloy composition in common.

For each property being compared, the top bar is H10 C65400 bronze and the bottom bar is H10 C68800 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 2.6
2.0
Poisson's Ratio 0.34
0.32
Rockwell B Hardness 100
99
Rockwell Superficial 30T Hardness 92
83
Shear Modulus, GPa 43
41
Shear Strength, MPa 530
510
Tensile Strength: Ultimate (UTS), MPa 930
890
Tensile Strength: Yield (Proof), MPa 910
790

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 24
17
Resilience: Unit (Modulus of Resilience), kJ/m3 3640
2860
Stiffness to Weight: Axial, points 7.3
7.3
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 30
30
Strength to Weight: Bending, points 24
25
Thermal Diffusivity, mm2/s 10
12
Thermal Shock Resistance, points 34
30

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