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7022 Aluminum vs. EN 1.7711 Steel

7022 aluminum belongs to the aluminum alloys classification, while EN 1.7711 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 1.7711 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 6.3 to 8.0
16 to 22
Fatigue Strength, MPa 140 to 170
290 to 520
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 290 to 320
440 to 570
Tensile Strength: Ultimate (UTS), MPa 490 to 540
690 to 930
Tensile Strength: Yield (Proof), MPa 390 to 460
400 to 800

Thermal Properties

Latent Heat of Fusion, J/g 380
250
Maximum Temperature: Mechanical, °C 200
430
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
33
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 65
8.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.0
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.5
2.3
Embodied Energy, MJ/kg 150
32
Embodied Water, L/kg 1130
54

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 40
130 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 1100 to 1500
430 to 1690
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 47 to 51
24 to 33
Strength to Weight: Bending, points 47 to 50
22 to 27
Thermal Diffusivity, mm2/s 54
8.9
Thermal Shock Resistance, points 21 to 23
24 to 32

Alloy Composition

Aluminum (Al), % 87.9 to 92.4
0 to 0.015
Carbon (C), % 0
0.36 to 0.44
Chromium (Cr), % 0.1 to 0.3
0.9 to 1.2
Copper (Cu), % 0.5 to 1.0
0
Iron (Fe), % 0 to 0.5
96 to 97.5
Magnesium (Mg), % 2.6 to 3.7
0
Manganese (Mn), % 0.1 to 0.4
0.45 to 0.85
Molybdenum (Mo), % 0
0.5 to 0.65
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.5
0 to 0.4
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Vanadium (V), % 0
0.25 to 0.35
Zinc (Zn), % 4.3 to 5.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0