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C66900 Brass vs. C37100 Brass

Both C66900 brass and C37100 brass are copper alloys. They have 84% 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 C66900 brass and the bottom bar is C37100 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
100
Elongation at Break, % 1.1 to 26
8.0 to 40
Poisson's Ratio 0.32
0.31
Rockwell Superficial 30T Hardness 60 to 88
43 to 71
Shear Modulus, GPa 45
40
Shear Strength, MPa 290 to 440
260 to 300
Tensile Strength: Ultimate (UTS), MPa 460 to 770
370 to 520
Tensile Strength: Yield (Proof), MPa 330 to 760
150 to 390

Thermal Properties

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

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
27
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
30

Otherwise Unclassified Properties

Base Metal Price, % relative 23
23
Density, g/cm3 8.2
8.0
Embodied Carbon, kg CO2/kg material 2.8
2.7
Embodied Energy, MJ/kg 46
45
Embodied Water, L/kg 310
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
38 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
110 to 750
Stiffness to Weight: Axial, points 8.1
7.2
Stiffness to Weight: Bending, points 20
20
Strength to Weight: Axial, points 15 to 26
13 to 18
Strength to Weight: Bending, points 16 to 23
14 to 18
Thermal Shock Resistance, points 14 to 23
12 to 17

Alloy Composition


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Copper (Cu), % 62.5 to 64.5
58 to 62
Iron (Fe), % 0 to 0.25
0 to 0.15
Lead (Pb), % 0 to 0.050
0.6 to 1.2
Manganese (Mn), % 11.5 to 12.5
0
Zinc (Zn), % 22.5 to 26
36.3 to 41.4
Residuals, % 0 to 0.2
0 to 0.4