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A380.0 Aluminum vs. SAE-AISI 4340 Steel

A380.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 A380.0 aluminum and the bottom bar is SAE-AISI 4340 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
210 to 360
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 3.3
12 to 22
Fatigue Strength, MPa 140
330 to 740
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
73
Shear Strength, MPa 190
430 to 770
Tensile Strength: Ultimate (UTS), MPa 290
690 to 1280
Tensile Strength: Yield (Proof), MPa 160
470 to 1150

Thermal Properties

Latent Heat of Fusion, J/g 510
250
Maximum Temperature: Mechanical, °C 170
430
Melting Completion (Liquidus), °C 590
1460
Melting Onset (Solidus), °C 550
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 96
44
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 78
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 11
3.5
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 7.5
1.7
Embodied Energy, MJ/kg 140
22
Embodied Water, L/kg 1040
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.3
79 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 180
590 to 3490
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 48
24
Strength to Weight: Axial, points 28
24 to 45
Strength to Weight: Bending, points 34
22 to 33
Thermal Diffusivity, mm2/s 38
12
Thermal Shock Resistance, points 13
20 to 38

Alloy Composition


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Aluminum (Al), % 80.3 to 89.5
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0
0.7 to 0.9
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 1.3
95.1 to 96.3
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.6 to 0.8
Molybdenum (Mo), % 0
0.2 to 0.3
Nickel (Ni), % 0 to 0.5
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 7.5 to 9.5
0.15 to 0.35
Sulfur (S), % 0
0 to 0.040
Tin (Sn), % 0 to 0.35
0
Zinc (Zn), % 0 to 3.0
0
Residuals, % 0 to 0.5
0