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H10 C26200 Brass vs. H10 C68800 Brass

Both H10 C26200 brass and H10 C68800 brass are copper alloys. Both are furnished in the H10 (extra spring) temper. They have a moderately high 91% 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 C68800 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 3.0
2.0
Poisson's Ratio 0.31
0.32
Rockwell B Hardness 93
99
Rockwell Superficial 30T Hardness 78
83
Shear Modulus, GPa 41
41
Shear Strength, MPa 390
510
Tensile Strength: Ultimate (UTS), MPa 680
890
Tensile Strength: Yield (Proof), MPa 490
790

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19
17
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
2860
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
25
Thermal Diffusivity, mm2/s 38
12
Thermal Shock Resistance, points 23
30

Alloy Composition


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Aluminum (Al), % 0
3.0 to 3.8
Cobalt (Co), % 0
0.25 to 0.55
Copper (Cu), % 67 to 70
70.8 to 75.5
Iron (Fe), % 0 to 0.050
0 to 0.2
Lead (Pb), % 0 to 0.070
0 to 0.050
Zinc (Zn), % 29.6 to 33
21.3 to 24.1
Residuals, % 0 to 0.3
0 to 0.5