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C34200 Brass vs. C68800 Brass

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

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

Aluminum (Al), % 0
3.0 to 3.8
Cobalt (Co), % 0
0.25 to 0.55
Copper (Cu), % 62 to 65
70.8 to 75.5
Iron (Fe), % 0 to 0.1
0 to 0.2
Lead (Pb), % 1.5 to 2.5
0 to 0.050
Zinc (Zn), % 32 to 36.5
21.3 to 24.1
Residuals, % 0
0 to 0.5

Comparable Variants