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C66900 Brass vs. C99750 Brass

Both C66900 brass and C99750 brass are copper alloys. They have a moderately high 90% of their average alloy composition in common. There are 27 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 C99750 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
130
Elongation at Break, % 1.1 to 26
20 to 30
Poisson's Ratio 0.32
0.32
Rockwell B Hardness 65 to 100
77 to 82
Shear Modulus, GPa 45
48
Tensile Strength: Ultimate (UTS), MPa 460 to 770
450 to 520
Tensile Strength: Yield (Proof), MPa 330 to 760
220 to 280

Thermal Properties

Latent Heat of Fusion, J/g 190
200
Maximum Temperature: Mechanical, °C 150
160
Melting Completion (Liquidus), °C 860
840
Melting Onset (Solidus), °C 850
820
Specific Heat Capacity, J/kg-K 400
410
Thermal Expansion, µm/m-K 20
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 23
23
Density, g/cm3 8.2
8.1
Embodied Carbon, kg CO2/kg material 2.8
3.1
Embodied Energy, MJ/kg 46
51
Embodied Water, L/kg 310
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
87 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
190 to 300
Stiffness to Weight: Axial, points 8.1
8.6
Stiffness to Weight: Bending, points 20
21
Strength to Weight: Axial, points 15 to 26
15 to 18
Strength to Weight: Bending, points 16 to 23
16 to 18
Thermal Shock Resistance, points 14 to 23
13 to 15

Alloy Composition

Aluminum (Al), % 0
0.25 to 3.0
Copper (Cu), % 62.5 to 64.5
55 to 61
Iron (Fe), % 0 to 0.25
0 to 1.0
Lead (Pb), % 0 to 0.050
0.5 to 2.5
Manganese (Mn), % 11.5 to 12.5
17 to 23
Nickel (Ni), % 0
0 to 5.0
Zinc (Zn), % 22.5 to 26
17 to 23
Residuals, % 0
0 to 0.3