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7022 Aluminum vs. S35115 Stainless Steel

7022 aluminum belongs to the aluminum alloys classification, while S35115 stainless steel belongs to the iron alloys. There are 30 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 7022 aluminum and the bottom bar is S35115 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 6.3 to 8.0
46
Fatigue Strength, MPa 140 to 170
280
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
79
Shear Strength, MPa 290 to 320
470
Tensile Strength: Ultimate (UTS), MPa 490 to 540
670
Tensile Strength: Yield (Proof), MPa 390 to 460
310

Thermal Properties

Latent Heat of Fusion, J/g 380
310
Maximum Temperature: Mechanical, °C 200
1100
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 480
1370
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140
15
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 21
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 65
2.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
26
Density, g/cm3 2.9
7.9
Embodied Carbon, kg CO2/kg material 8.5
4.8
Embodied Energy, MJ/kg 150
67
Embodied Water, L/kg 1130
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 40
250
Resilience: Unit (Modulus of Resilience), kJ/m3 1100 to 1500
240
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 47 to 51
24
Strength to Weight: Bending, points 47 to 50
22
Thermal Diffusivity, mm2/s 54
3.9
Thermal Shock Resistance, points 21 to 23
15

Alloy Composition

Aluminum (Al), % 87.9 to 92.4
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0.1 to 0.3
23 to 25
Copper (Cu), % 0.5 to 1.0
0
Iron (Fe), % 0 to 0.5
47.6 to 55.8
Magnesium (Mg), % 2.6 to 3.7
0
Manganese (Mn), % 0.1 to 0.4
0 to 1.0
Molybdenum (Mo), % 0
1.5 to 2.5
Nickel (Ni), % 0
19 to 22
Nitrogen (N), % 0
0.2 to 0.3
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.5
0.5 to 1.5
Sulfur (S), % 0
0 to 0.015
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