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C66900 Brass vs. SAE-AISI 1086 Steel

C66900 brass belongs to the copper alloys classification, while SAE-AISI 1086 steel belongs to the iron alloys. There are 27 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is C66900 brass and the bottom bar is SAE-AISI 1086 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
190
Elongation at Break, % 1.1 to 26
11
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 45
72
Shear Strength, MPa 290 to 440
450 to 520
Tensile Strength: Ultimate (UTS), MPa 460 to 770
760 to 870
Tensile Strength: Yield (Proof), MPa 330 to 760
480 to 580

Thermal Properties

Latent Heat of Fusion, J/g 190
240
Maximum Temperature: Mechanical, °C 150
400
Melting Completion (Liquidus), °C 860
1460
Melting Onset (Solidus), °C 850
1410
Specific Heat Capacity, J/kg-K 400
470
Thermal Expansion, µm/m-K 20
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
7.0
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
8.1

Otherwise Unclassified Properties

Base Metal Price, % relative 23
1.8
Density, g/cm3 8.2
7.8
Embodied Carbon, kg CO2/kg material 2.8
1.4
Embodied Energy, MJ/kg 46
19
Embodied Water, L/kg 310
45

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
79 to 84
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
610 to 890
Stiffness to Weight: Axial, points 8.1
13
Stiffness to Weight: Bending, points 20
24
Strength to Weight: Axial, points 15 to 26
27 to 31
Strength to Weight: Bending, points 16 to 23
24 to 26
Thermal Shock Resistance, points 14 to 23
26 to 30

Alloy Composition

Carbon (C), % 0
0.8 to 0.93
Copper (Cu), % 62.5 to 64.5
0
Iron (Fe), % 0 to 0.25
98.5 to 98.9
Lead (Pb), % 0 to 0.050
0
Manganese (Mn), % 11.5 to 12.5
0.3 to 0.5
Phosphorus (P), % 0
0 to 0.040
Sulfur (S), % 0
0 to 0.050
Zinc (Zn), % 22.5 to 26
0
Residuals, % 0 to 0.2
0