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C68800 Brass vs. C26200 Brass

Both C68800 brass and C26200 brass are copper alloys. They have a moderately high 91% of their average alloy composition in common.

For each property being compared, the top bar is C68800 brass and the bottom bar is C26200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 2.0 to 36
3.0 to 180
Poisson's Ratio 0.32
0.31
Rockwell B Hardness 81 to 99
55 to 93
Rockwell Superficial 30T Hardness 71 to 83
26 to 78
Shear Modulus, GPa 41
41
Shear Strength, MPa 380 to 510
230 to 390
Tensile Strength: Ultimate (UTS), MPa 570 to 890
330 to 770
Tensile Strength: Yield (Proof), MPa 390 to 790
110 to 490

Thermal Properties

Latent Heat of Fusion, J/g 190
180
Maximum Temperature: Mechanical, °C 160
140
Melting Completion (Liquidus), °C 960
950
Melting Onset (Solidus), °C 950
920
Specific Heat Capacity, J/kg-K 400
390
Thermal Conductivity, W/m-K 40
120
Thermal Expansion, µm/m-K 19
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 18
28
Electrical Conductivity: Equal Weight (Specific), % IACS 20
31

Otherwise Unclassified Properties

Base Metal Price, % relative 26
25
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.7
Embodied Energy, MJ/kg 48
45
Embodied Water, L/kg 350
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 180
19 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 710 to 2860
62 to 1110
Stiffness to Weight: Axial, points 7.3
7.2
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 19 to 30
11 to 26
Strength to Weight: Bending, points 19 to 25
13 to 23
Thermal Diffusivity, mm2/s 12
38
Thermal Shock Resistance, points 19 to 30
11 to 26

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
67 to 70
Iron (Fe), % 0 to 0.2
0 to 0.050
Lead (Pb), % 0 to 0.050
0 to 0.070
Zinc (Zn), % 21.3 to 24.1
29.6 to 33
Residuals, % 0
0 to 0.3

Comparable Variants