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C68800 Brass vs. C34200 Brass

Both C68800 brass and C34200 brass are copper alloys. They have 86% of their average alloy composition in common.

For each property being compared, the top bar is C68800 brass and the bottom bar is C34200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
100
Elongation at Break, % 2.0 to 36
3.0 to 17
Poisson's Ratio 0.32
0.31
Rockwell B Hardness 81 to 99
53 to 91
Rockwell Superficial 30T Hardness 71 to 83
52 to 78
Shear Modulus, GPa 41
40
Shear Strength, MPa 380 to 510
230 to 360
Tensile Strength: Ultimate (UTS), MPa 570 to 890
370 to 650
Tensile Strength: Yield (Proof), MPa 390 to 790
150 to 420

Thermal Properties

Latent Heat of Fusion, J/g 190
170
Maximum Temperature: Mechanical, °C 160
120
Melting Completion (Liquidus), °C 960
910
Melting Onset (Solidus), °C 950
890
Specific Heat Capacity, J/kg-K 400
380
Thermal Conductivity, W/m-K 40
120
Thermal Expansion, µm/m-K 19
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 18
26
Electrical Conductivity: Equal Weight (Specific), % IACS 20
29

Otherwise Unclassified Properties

Base Metal Price, % relative 26
24
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.6
Embodied Energy, MJ/kg 48
45
Embodied Water, L/kg 350
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 180
9.0 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 710 to 2860
110 to 870
Stiffness to Weight: Axial, points 7.3
7.1
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 19 to 30
13 to 22
Strength to Weight: Bending, points 19 to 25
14 to 20
Thermal Diffusivity, mm2/s 12
37
Thermal Shock Resistance, points 19 to 30
12 to 22

Alloy Composition

Aluminum (Al), % 3.0 to 3.8
0
Cobalt (Co), % 0.25 to 0.55
0
Copper (Cu), % 70.8 to 75.5
62 to 65
Iron (Fe), % 0 to 0.2
0 to 0.1
Lead (Pb), % 0 to 0.050
1.5 to 2.5
Zinc (Zn), % 21.3 to 24.1
32 to 36.5
Residuals, % 0
0 to 0.4

Comparable Variants