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C66900 Brass vs. C27200 Brass

Both C66900 brass and C27200 brass are copper alloys. They have 88% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.

For each property being compared, the top bar is C66900 brass and the bottom bar is C27200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 1.1 to 26
10 to 50
Poisson's Ratio 0.32
0.31
Rockwell B Hardness 65 to 100
53 to 86
Shear Modulus, GPa 45
40
Shear Strength, MPa 290 to 440
230 to 320
Tensile Strength: Ultimate (UTS), MPa 460 to 770
370 to 590
Tensile Strength: Yield (Proof), MPa 330 to 760
150 to 410

Thermal Properties

Latent Heat of Fusion, J/g 190
170
Maximum Temperature: Mechanical, °C 150
130
Melting Completion (Liquidus), °C 860
920
Melting Onset (Solidus), °C 850
870
Specific Heat Capacity, J/kg-K 400
390
Thermal Expansion, µm/m-K 20
20

Electrical Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 23
24
Density, g/cm3 8.2
8.1
Embodied Carbon, kg CO2/kg material 2.8
2.7
Embodied Energy, MJ/kg 46
45
Embodied Water, L/kg 310
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
30 to 270
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
110 to 810
Stiffness to Weight: Axial, points 8.1
7.2
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 15 to 26
13 to 20
Strength to Weight: Bending, points 16 to 23
14 to 19
Thermal Shock Resistance, points 14 to 23
12 to 20

Alloy Composition

Copper (Cu), % 62.5 to 64.5
62 to 65
Iron (Fe), % 0 to 0.25
0 to 0.070
Lead (Pb), % 0 to 0.050
0 to 0.070
Manganese (Mn), % 11.5 to 12.5
0
Zinc (Zn), % 22.5 to 26
34.6 to 38
Residuals, % 0
0 to 0.3

Comparable Variants