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C66200 Brass vs. C66900 Brass

Both C66200 brass and C66900 brass are copper alloys. They have 73% of their average alloy composition in common. There are 27 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is C66200 brass and the bottom bar is C66900 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 8.0 to 15
1.1 to 26
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 42
45
Shear Strength, MPa 270 to 300
290 to 440
Tensile Strength: Ultimate (UTS), MPa 450 to 520
460 to 770
Tensile Strength: Yield (Proof), MPa 410 to 480
330 to 760

Thermal Properties

Latent Heat of Fusion, J/g 200
190
Maximum Temperature: Mechanical, °C 180
150
Melting Completion (Liquidus), °C 1070
860
Melting Onset (Solidus), °C 1030
850
Specific Heat Capacity, J/kg-K 390
400
Thermal Expansion, µm/m-K 18
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 36
3.8

Otherwise Unclassified Properties

Base Metal Price, % relative 29
23
Density, g/cm3 8.7
8.2
Embodied Carbon, kg CO2/kg material 2.7
2.8
Embodied Energy, MJ/kg 43
46
Embodied Water, L/kg 320
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
4.6 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
460 to 2450
Stiffness to Weight: Axial, points 7.2
8.1
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 14 to 17
15 to 26
Strength to Weight: Bending, points 15 to 16
16 to 23
Thermal Shock Resistance, points 16 to 18
14 to 23

Alloy Composition

Copper (Cu), % 86.6 to 91
62.5 to 64.5
Iron (Fe), % 0 to 0.050
0 to 0.25
Lead (Pb), % 0 to 0.050
0 to 0.050
Manganese (Mn), % 0
11.5 to 12.5
Nickel (Ni), % 0.3 to 1.0
0
Phosphorus (P), % 0.050 to 0.2
0
Tin (Sn), % 0.2 to 0.7
0
Zinc (Zn), % 6.5 to 12.9
22.5 to 26
Residuals, % 0
0 to 0.2