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7022 Aluminum vs. EN 1.5508 Steel

7022 aluminum belongs to the aluminum alloys classification, while EN 1.5508 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 7022 aluminum and the bottom bar is EN 1.5508 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 6.3 to 8.0
11 to 20
Fatigue Strength, MPa 140 to 170
210 to 320
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 290 to 320
300 to 360
Tensile Strength: Ultimate (UTS), MPa 490 to 540
420 to 1460
Tensile Strength: Yield (Proof), MPa 390 to 460
310 to 490

Thermal Properties

Latent Heat of Fusion, J/g 380
250
Maximum Temperature: Mechanical, °C 200
400
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 480
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 140
51
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
7.1
Electrical Conductivity: Equal Weight (Specific), % IACS 65
8.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
1.9
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.5
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1130
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 40
44 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 1100 to 1500
260 to 640
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 47 to 51
15 to 52
Strength to Weight: Bending, points 47 to 50
16 to 36
Thermal Diffusivity, mm2/s 54
14
Thermal Shock Resistance, points 21 to 23
12 to 43

Alloy Composition

Aluminum (Al), % 87.9 to 92.4
0
Boron (B), % 0
0.00080 to 0.0050
Carbon (C), % 0
0.2 to 0.25
Chromium (Cr), % 0.1 to 0.3
0 to 0.3
Copper (Cu), % 0.5 to 1.0
0 to 0.25
Iron (Fe), % 0 to 0.5
97.9 to 99.199
Magnesium (Mg), % 2.6 to 3.7
0
Manganese (Mn), % 0.1 to 0.4
0.6 to 0.9
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.5
0 to 0.3
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 4.3 to 5.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0