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C26200 Brass vs. C65400 Bronze

Both C26200 brass and C65400 bronze are copper alloys. They have 69% of their average alloy composition in common.

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

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 3.0 to 180
2.6 to 47
Poisson's Ratio 0.31
0.34
Rockwell B Hardness 55 to 93
82 to 120
Rockwell Superficial 30T Hardness 26 to 78
71 to 92
Shear Modulus, GPa 41
43
Shear Strength, MPa 230 to 390
350 to 530
Tensile Strength: Ultimate (UTS), MPa 330 to 770
500 to 1060
Tensile Strength: Yield (Proof), MPa 110 to 490
170 to 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 to 160
10 to 480
Resilience: Unit (Modulus of Resilience), kJ/m3 62 to 1110
130 to 3640
Stiffness to Weight: Axial, points 7.2
7.3
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 11 to 26
16 to 34
Strength to Weight: Bending, points 13 to 23
16 to 27
Thermal Diffusivity, mm2/s 38
10
Thermal Shock Resistance, points 11 to 26
18 to 39

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

Comparable Variants