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H01 C26200 Brass vs. H01 C66900 Brass

Both H01 C26200 brass and H01 C66900 brass are copper alloys. Both are furnished in the H01 (quarter hard) temper. They have 88% 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 C26200 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, % 32
26
Poisson's Ratio 0.31
0.32
Rockwell B Hardness 55
65
Rockwell Superficial 30T Hardness 54
60
Shear Modulus, GPa 41
45
Shear Strength, MPa 250
290
Tensile Strength: Ultimate (UTS), MPa 430
460
Tensile Strength: Yield (Proof), MPa 300
330

Thermal Properties

Latent Heat of Fusion, J/g 180
190
Maximum Temperature: Mechanical, °C 140
150
Melting Completion (Liquidus), °C 950
860
Melting Onset (Solidus), °C 920
850
Specific Heat Capacity, J/kg-K 390
400
Thermal Expansion, µm/m-K 20
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 31
3.8

Otherwise Unclassified Properties

Base Metal Price, % relative 25
23
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 2.7
2.8
Embodied Energy, MJ/kg 45
46
Embodied Water, L/kg 320
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
110
Resilience: Unit (Modulus of Resilience), kJ/m3 420
460
Stiffness to Weight: Axial, points 7.2
8.1
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 14
15
Strength to Weight: Bending, points 15
16
Thermal Shock Resistance, points 14
14

Alloy Composition

Copper (Cu), % 67 to 70
62.5 to 64.5
Iron (Fe), % 0 to 0.050
0 to 0.25
Lead (Pb), % 0 to 0.070
0 to 0.050
Manganese (Mn), % 0
11.5 to 12.5
Zinc (Zn), % 29.6 to 33
22.5 to 26
Residuals, % 0
0 to 0.2