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H10 C26200 Brass vs. H10 C65400 Bronze

Both H10 C26200 brass and H10 C65400 bronze are copper alloys. Both are furnished in the H10 (extra spring) temper. They have 69% of their average alloy composition in common.

For each property being compared, the top bar is H10 C26200 brass and the bottom bar is H10 C65400 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 3.0
2.6
Poisson's Ratio 0.31
0.34
Rockwell B Hardness 93
100
Rockwell Superficial 30T Hardness 78
92
Shear Modulus, GPa 41
43
Shear Strength, MPa 390
530
Tensile Strength: Ultimate (UTS), MPa 680
930
Tensile Strength: Yield (Proof), MPa 490
910

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: Ultimate (Unit Rupture Work), MJ/m3 19
24
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
3640
Stiffness to Weight: Axial, points 7.2
7.3
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 23
30
Strength to Weight: Bending, points 21
24
Thermal Diffusivity, mm2/s 38
10
Thermal Shock Resistance, points 23
34

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