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H08 C66900 Brass vs. H08 C68800 Brass

Both H08 C66900 brass and H08 C68800 brass are copper alloys. Both are furnished in the H08 (spring) temper. They have 86% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is H08 C66900 brass and the bottom bar is H08 C68800 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 3.0
2.0
Poisson's Ratio 0.32
0.32
Rockwell B Hardness 92
98
Rockwell Superficial 30T Hardness 79
83
Shear Modulus, GPa 45
41
Shear Strength, MPa 400
480
Tensile Strength: Ultimate (UTS), MPa 690
840

Thermal Properties

Latent Heat of Fusion, J/g 190
190
Maximum Temperature: Mechanical, °C 150
160
Melting Completion (Liquidus), °C 860
960
Melting Onset (Solidus), °C 850
950
Specific Heat Capacity, J/kg-K 400
400
Thermal Expansion, µm/m-K 20
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
18
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
20

Otherwise Unclassified Properties

Base Metal Price, % relative 23
26
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.8
Embodied Energy, MJ/kg 46
48
Embodied Water, L/kg 310
350

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
16
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
2670
Stiffness to Weight: Axial, points 8.1
7.3
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 23
29
Strength to Weight: Bending, points 21
24
Thermal Shock Resistance, points 21
29

Alloy Composition

Aluminum (Al), % 0
3.0 to 3.8
Cobalt (Co), % 0
0.25 to 0.55
Copper (Cu), % 62.5 to 64.5
70.8 to 75.5
Iron (Fe), % 0 to 0.25
0 to 0.2
Lead (Pb), % 0 to 0.050
0 to 0.050
Manganese (Mn), % 11.5 to 12.5
0
Zinc (Zn), % 22.5 to 26
21.3 to 24.1
Residuals, % 0
0 to 0.5