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H01 C41500 Brass vs. H01 C66900 Brass

Both H01 C41500 brass and H01 C66900 brass are copper alloys. Both are furnished in the H01 (quarter hard) temper. They have 71% 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 H01 C41500 brass and the bottom bar is H01 C66900 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 28
26
Poisson's Ratio 0.33
0.32
Rockwell B Hardness 62
65
Rockwell Superficial 30T Hardness 58
60
Shear Modulus, GPa 42
45
Shear Strength, MPa 220
290
Tensile Strength: Ultimate (UTS), MPa 340
460
Tensile Strength: Yield (Proof), MPa 310
330

Thermal Properties

Latent Heat of Fusion, J/g 200
190
Maximum Temperature: Mechanical, °C 180
150
Melting Completion (Liquidus), °C 1030
860
Melting Onset (Solidus), °C 1010
850
Specific Heat Capacity, J/kg-K 380
400
Thermal Expansion, µm/m-K 18
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 29
3.8

Otherwise Unclassified Properties

Base Metal Price, % relative 30
23
Density, g/cm3 8.7
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.8
Embodied Energy, MJ/kg 45
46
Embodied Water, L/kg 330
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 93
110
Resilience: Unit (Modulus of Resilience), kJ/m3 420
460
Stiffness to Weight: Axial, points 7.1
8.1
Stiffness to Weight: Bending, points 18
20
Strength to Weight: Axial, points 11
15
Strength to Weight: Bending, points 12
16
Thermal Shock Resistance, points 12
14

Alloy Composition


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Copper (Cu), % 89 to 93
62.5 to 64.5
Iron (Fe), % 0 to 0.050
0 to 0.25
Lead (Pb), % 0 to 0.1
0 to 0.050
Manganese (Mn), % 0
11.5 to 12.5
Tin (Sn), % 1.5 to 2.2
0
Zinc (Zn), % 4.2 to 9.5
22.5 to 26
Residuals, % 0 to 0.5
0 to 0.2