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5383 Aluminum vs. SAE-AISI 4340M Steel

5383 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340M steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 5383 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 110
710
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.7 to 15
6.0
Fatigue Strength, MPa 130 to 200
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 190 to 220
1360
Tensile Strength: Ultimate (UTS), MPa 310 to 370
2340
Tensile Strength: Yield (Proof), MPa 150 to 310
1240

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Mechanical, °C 200
430
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 540
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
38
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 97
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.9
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
1.9
Embodied Energy, MJ/kg 160
26
Embodied Water, L/kg 1170
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
120
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 32 to 38
84
Strength to Weight: Bending, points 38 to 42
51
Thermal Diffusivity, mm2/s 51
10
Thermal Shock Resistance, points 14 to 16
70

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0 to 0.25
0.7 to 1.0
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.25
93.3 to 94.8
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 0
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 0 to 0.25
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.15
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0