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C55180 Copper vs. C99700 Brass

Both C55180 copper and C99700 brass are copper alloys. Both are furnished in the as-fabricated (no temper or treatment) condition. They have 60% of their average alloy composition in common. There are 24 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is C55180 copper and the bottom bar is C99700 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 20
25
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 41
46
Tensile Strength: Ultimate (UTS), MPa 200
380
Tensile Strength: Yield (Proof), MPa 100
170

Thermal Properties

Latent Heat of Fusion, J/g 200
200
Maximum Temperature: Mechanical, °C 200
160
Melting Completion (Liquidus), °C 920
900
Melting Onset (Solidus), °C 710
880
Specific Heat Capacity, J/kg-K 400
410
Thermal Expansion, µm/m-K 17
20

Otherwise Unclassified Properties

Base Metal Price, % relative 29
25
Density, g/cm3 8.6
8.1
Embodied Carbon, kg CO2/kg material 2.5
3.3
Embodied Energy, MJ/kg 39
53
Embodied Water, L/kg 290
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 34
78
Resilience: Unit (Modulus of Resilience), kJ/m3 48
120
Stiffness to Weight: Axial, points 7.1
8.3
Stiffness to Weight: Bending, points 18
20
Strength to Weight: Axial, points 6.4
13
Strength to Weight: Bending, points 8.8
14
Thermal Shock Resistance, points 7.9
11

Alloy Composition


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Aluminum (Al), % 0
0.5 to 3.0
Copper (Cu), % 94.7 to 95.2
54 to 65.5
Iron (Fe), % 0
0 to 1.0
Lead (Pb), % 0
0 to 2.0
Manganese (Mn), % 0
11 to 15
Nickel (Ni), % 0
4.0 to 6.0
Phosphorus (P), % 4.8 to 5.2
0
Tin (Sn), % 0
0 to 1.0
Zinc (Zn), % 0
19 to 25
Residuals, % 0 to 0.15
0 to 0.3