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C36200 Brass vs. C66900 Brass

Both C36200 brass and C66900 brass are copper alloys. They have 86% 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 C36200 brass and the bottom bar is C66900 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
120
Elongation at Break, % 20 to 53
1.1 to 26
Poisson's Ratio 0.31
0.32
Rockwell B Hardness 62 to 78
65 to 100
Shear Modulus, GPa 39
45
Shear Strength, MPa 210 to 240
290 to 440
Tensile Strength: Ultimate (UTS), MPa 340 to 420
460 to 770
Tensile Strength: Yield (Proof), MPa 130 to 360
330 to 760

Thermal Properties

Latent Heat of Fusion, J/g 170
190
Maximum Temperature: Mechanical, °C 120
150
Melting Completion (Liquidus), °C 900
860
Melting Onset (Solidus), °C 890
850
Specific Heat Capacity, J/kg-K 380
400
Thermal Expansion, µm/m-K 21
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 28
3.8

Otherwise Unclassified Properties

Base Metal Price, % relative 23
23
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 2.6
2.8
Embodied Energy, MJ/kg 45
46
Embodied Water, L/kg 320
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 140
4.6 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 89 to 630
460 to 2450
Stiffness to Weight: Axial, points 6.9
8.1
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 11 to 14
15 to 26
Strength to Weight: Bending, points 13 to 15
16 to 23
Thermal Shock Resistance, points 11 to 14
14 to 23

Alloy Composition

Copper (Cu), % 60 to 63
62.5 to 64.5
Iron (Fe), % 0 to 0.15
0 to 0.25
Lead (Pb), % 3.5 to 4.5
0 to 0.050
Manganese (Mn), % 0
11.5 to 12.5
Zinc (Zn), % 32.4 to 36.5
22.5 to 26
Residuals, % 0
0 to 0.2

Comparable Variants