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H02 C66900 Brass vs. H02 C68800 Brass

Both H02 C66900 brass and H02 C68800 brass are copper alloys. Both are furnished in the H02 (half hard) temper. They have 86% of their average alloy composition in common. There are 29 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is H02 C66900 brass and the bottom bar is H02 C68800 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 16
20
Poisson's Ratio 0.32
0.32
Rockwell B Hardness 79
90
Rockwell Superficial 30T Hardness 71
78
Shear Modulus, GPa 45
41
Shear Strength, MPa 310
400
Tensile Strength: Ultimate (UTS), MPa 500
640
Tensile Strength: Yield (Proof), MPa 410
520

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 76
120
Resilience: Unit (Modulus of Resilience), kJ/m3 720
1240
Stiffness to Weight: Axial, points 8.1
7.3
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 17
22
Strength to Weight: Bending, points 17
20
Thermal Shock Resistance, points 15
22

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