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H04 C66900 Brass vs. H04 C68800 Brass

Both H04 C66900 brass and H04 C68800 brass are copper alloys. Both are furnished in the H04 (full 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 H04 C66900 brass and the bottom bar is H04 C68800 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 5.0
6.0
Poisson's Ratio 0.32
0.32
Rockwell B Hardness 88
96
Rockwell Superficial 30T Hardness 77
82
Shear Modulus, GPa 45
41
Shear Strength, MPa 360
440
Tensile Strength: Ultimate (UTS), MPa 610
750
Tensile Strength: Yield (Proof), MPa 590
670

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 30
43
Resilience: Unit (Modulus of Resilience), kJ/m3 1480
2070
Stiffness to Weight: Axial, points 8.1
7.3
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 21
26
Strength to Weight: Bending, points 20
22
Thermal Shock Resistance, points 18
26

Alloy Composition


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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 to 0.2
0 to 0.5