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7020 Aluminum vs. SAE-AISI 4340M Steel

7020 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 (4, 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 7020 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 45 to 100
710
Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 8.4 to 14
6.0
Fatigue Strength, MPa 110 to 130
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 110 to 230
1360
Tensile Strength: Ultimate (UTS), MPa 190 to 390
2340
Tensile Strength: Yield (Proof), MPa 120 to 310
1240

Thermal Properties

Latent Heat of Fusion, J/g 380
280
Maximum Temperature: Mechanical, °C 210
430
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 610
1400
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 150
38
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 39
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 120
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.9
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1150
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 46
120
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 690
4120
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 18 to 37
84
Strength to Weight: Bending, points 25 to 41
51
Thermal Diffusivity, mm2/s 59
10
Thermal Shock Resistance, points 8.3 to 17
70

Alloy Composition

Aluminum (Al), % 91.2 to 94.8
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0.1 to 0.35
0.7 to 1.0
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.4
93.3 to 94.8
Magnesium (Mg), % 1.0 to 1.4
0
Manganese (Mn), % 0.050 to 0.5
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 0.35
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 4.0 to 5.0
0
Zirconium (Zr), % 0.080 to 0.25
0
Residuals, % 0 to 0.15
0