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C66900 Brass vs. C17200 Copper

Both C66900 brass and C17200 copper are copper alloys. They have 64% of their average alloy composition in common. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is C66900 brass and the bottom bar is C17200 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
120
Elongation at Break, % 1.1 to 26
1.1 to 37
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 45
45
Shear Strength, MPa 290 to 440
330 to 780
Tensile Strength: Ultimate (UTS), MPa 460 to 770
480 to 1380
Tensile Strength: Yield (Proof), MPa 330 to 760
160 to 1250

Thermal Properties

Latent Heat of Fusion, J/g 190
230
Maximum Temperature: Mechanical, °C 150
280
Melting Completion (Liquidus), °C 860
980
Melting Onset (Solidus), °C 850
870
Specific Heat Capacity, J/kg-K 400
390
Thermal Expansion, µm/m-K 20
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
22
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
23

Otherwise Unclassified Properties

Density, g/cm3 8.2
8.8
Embodied Carbon, kg CO2/kg material 2.8
9.4
Embodied Energy, MJ/kg 46
150
Embodied Water, L/kg 310
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
4.2 to 500
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
110 to 5720
Stiffness to Weight: Axial, points 8.1
7.6
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 15 to 26
15 to 44
Strength to Weight: Bending, points 16 to 23
16 to 31
Thermal Shock Resistance, points 14 to 23
16 to 46

Alloy Composition

Aluminum (Al), % 0
0 to 0.2
Beryllium (Be), % 0
1.8 to 2.0
Copper (Cu), % 62.5 to 64.5
96.1 to 98
Iron (Fe), % 0 to 0.25
0 to 0.4
Lead (Pb), % 0 to 0.050
0
Manganese (Mn), % 11.5 to 12.5
0
Nickel (Ni), % 0
0.2 to 0.6
Silicon (Si), % 0
0 to 0.2
Zinc (Zn), % 22.5 to 26
0
Residuals, % 0
0 to 0.5