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C68100 Brass vs. C36200 Brass

Both C68100 brass and C36200 brass are copper alloys. They have a moderately high 93% 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 C68100 brass and the bottom bar is C36200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
100
Elongation at Break, % 29
20 to 53
Poisson's Ratio 0.3
0.31
Shear Modulus, GPa 40
39
Tensile Strength: Ultimate (UTS), MPa 380
340 to 420
Tensile Strength: Yield (Proof), MPa 140
130 to 360

Thermal Properties

Latent Heat of Fusion, J/g 170
170
Maximum Temperature: Mechanical, °C 120
120
Melting Completion (Liquidus), °C 890
900
Melting Onset (Solidus), °C 870
890
Specific Heat Capacity, J/kg-K 390
380
Thermal Conductivity, W/m-K 98
120
Thermal Expansion, µm/m-K 21
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
26
Electrical Conductivity: Equal Weight (Specific), % IACS 27
28

Otherwise Unclassified Properties

Base Metal Price, % relative 23
23
Density, g/cm3 7.9
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.6
Embodied Energy, MJ/kg 47
45
Embodied Water, L/kg 330
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 86
74 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 94
89 to 630
Stiffness to Weight: Axial, points 7.3
6.9
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 13
11 to 14
Strength to Weight: Bending, points 15
13 to 15
Thermal Diffusivity, mm2/s 32
37
Thermal Shock Resistance, points 13
11 to 14

Alloy Composition


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Aluminum (Al), % 0 to 0.010
0
Copper (Cu), % 56 to 60
60 to 63
Iron (Fe), % 0.25 to 1.3
0 to 0.15
Lead (Pb), % 0 to 0.050
3.5 to 4.5
Manganese (Mn), % 0.010 to 0.5
0
Silicon (Si), % 0.040 to 0.15
0
Tin (Sn), % 0.75 to 1.1
0
Zinc (Zn), % 36.4 to 43
32.4 to 36.5
Residuals, % 0 to 0.5
0