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7050 Aluminum vs. SAE-AISI 4340 Steel

7050 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340 steel belongs to the iron alloys. There are 30 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 7050 aluminum and the bottom bar is SAE-AISI 4340 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2 to 12
12 to 22
Fatigue Strength, MPa 130 to 210
330 to 740
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 280 to 330
430 to 770
Tensile Strength: Ultimate (UTS), MPa 490 to 570
690 to 1280
Tensile Strength: Yield (Proof), MPa 390 to 500
470 to 1150

Thermal Properties

Latent Heat of Fusion, J/g 370
250
Maximum Temperature: Mechanical, °C 190
430
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 490
1420
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 140
44
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.5
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
1.7
Embodied Energy, MJ/kg 150
22
Embodied Water, L/kg 1120
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
79 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
590 to 3490
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 45 to 51
24 to 45
Strength to Weight: Bending, points 45 to 50
22 to 33
Thermal Diffusivity, mm2/s 54
12
Thermal Shock Resistance, points 21 to 25
20 to 38

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0 to 0.040
0.7 to 0.9
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
95.1 to 96.3
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0.6 to 0.8
Molybdenum (Mo), % 0
0.2 to 0.3
Nickel (Ni), % 0
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.12
0.15 to 0.35
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0