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C66900 Brass vs. SAE-AISI 1140 Steel

C66900 brass belongs to the copper alloys classification, while SAE-AISI 1140 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 1140 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
190
Elongation at Break, % 1.1 to 26
14 to 18
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 45
72
Shear Strength, MPa 290 to 440
370 to 420
Tensile Strength: Ultimate (UTS), MPa 460 to 770
600 to 700
Tensile Strength: Yield (Proof), MPa 330 to 760
340 to 570

Thermal Properties

Latent Heat of Fusion, J/g 190
250
Maximum Temperature: Mechanical, °C 150
400
Melting Completion (Liquidus), °C 860
1460
Melting Onset (Solidus), °C 850
1420
Specific Heat Capacity, J/kg-K 400
470
Thermal Expansion, µm/m-K 20
13

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
18
Embodied Water, L/kg 310
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
89 to 93
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
310 to 870
Stiffness to Weight: Axial, points 8.1
13
Stiffness to Weight: Bending, points 20
24
Strength to Weight: Axial, points 15 to 26
21 to 25
Strength to Weight: Bending, points 16 to 23
20 to 22
Thermal Shock Resistance, points 14 to 23
18 to 21

Alloy Composition

Carbon (C), % 0
0.37 to 0.44
Copper (Cu), % 62.5 to 64.5
0
Iron (Fe), % 0 to 0.25
98.4 to 98.9
Lead (Pb), % 0 to 0.050
0
Manganese (Mn), % 11.5 to 12.5
0.7 to 1.0
Phosphorus (P), % 0
0 to 0.040
Sulfur (S), % 0
0.080 to 0.13
Zinc (Zn), % 22.5 to 26
0
Residuals, % 0 to 0.2
0