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7022 Aluminum vs. S17400 Stainless Steel

7022 aluminum belongs to the aluminum alloys classification, while S17400 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 S17400 stainless 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 21
Fatigue Strength, MPa 140 to 170
380 to 670
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
75
Shear Strength, MPa 290 to 320
570 to 830
Tensile Strength: Ultimate (UTS), MPa 490 to 540
910 to 1390
Tensile Strength: Yield (Proof), MPa 390 to 460
580 to 1250

Thermal Properties

Latent Heat of Fusion, J/g 380
280
Maximum Temperature: Mechanical, °C 200
850
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 480
1400
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140
17
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 65
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 10
14
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.5
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1130
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 40
140 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 1100 to 1500
880 to 4060
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 47 to 51
32 to 49
Strength to Weight: Bending, points 47 to 50
27 to 35
Thermal Diffusivity, mm2/s 54
4.5
Thermal Shock Resistance, points 21 to 23
30 to 46

Alloy Composition

Aluminum (Al), % 87.9 to 92.4
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0.1 to 0.3
15 to 17
Copper (Cu), % 0.5 to 1.0
3.0 to 5.0
Iron (Fe), % 0 to 0.5
70.4 to 78.9
Magnesium (Mg), % 2.6 to 3.7
0
Manganese (Mn), % 0.1 to 0.4
0 to 1.0
Nickel (Ni), % 0
3.0 to 5.0
Niobium (Nb), % 0
0.15 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
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