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SAE-AISI 1140 Steel vs. C66900 Brass

SAE-AISI 1140 steel belongs to the iron alloys classification, while C66900 brass belongs to the copper 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 SAE-AISI 1140 steel and the bottom bar is C66900 brass.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
23
Density, g/cm3 7.8
8.2
Embodied Carbon, kg CO2/kg material 1.4
2.8
Embodied Energy, MJ/kg 18
46
Embodied Water, L/kg 46
310

Common Calculations

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

Alloy Composition

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