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EN 1.4606 Stainless Steel vs. 7022 Aluminum

EN 1.4606 stainless steel belongs to the iron alloys classification, while 7022 aluminum belongs to the aluminum 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 EN 1.4606 stainless steel and the bottom bar is 7022 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 23 to 39
6.3 to 8.0
Fatigue Strength, MPa 240 to 420
140 to 170
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 75
26
Shear Strength, MPa 410 to 640
290 to 320
Tensile Strength: Ultimate (UTS), MPa 600 to 1020
490 to 540
Tensile Strength: Yield (Proof), MPa 280 to 630
390 to 460

Thermal Properties

Latent Heat of Fusion, J/g 300
380
Maximum Temperature: Mechanical, °C 910
200
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
480
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 14
140
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
21
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
65

Otherwise Unclassified Properties

Base Metal Price, % relative 26
10
Density, g/cm3 7.9
2.9
Embodied Carbon, kg CO2/kg material 6.0
8.5
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 170
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190 to 200
29 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 1010
1100 to 1500
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
47
Strength to Weight: Axial, points 21 to 36
47 to 51
Strength to Weight: Bending, points 20 to 28
47 to 50
Thermal Diffusivity, mm2/s 3.7
54
Thermal Shock Resistance, points 21 to 35
21 to 23

Alloy Composition

Aluminum (Al), % 0 to 0.35
87.9 to 92.4
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13 to 16
0.1 to 0.3
Copper (Cu), % 0
0.5 to 1.0
Iron (Fe), % 49.2 to 59
0 to 0.5
Magnesium (Mg), % 0
2.6 to 3.7
Manganese (Mn), % 1.0 to 2.0
0.1 to 0.4
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 1.0
0 to 0.5
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.9 to 2.3
0 to 0.2
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
4.3 to 5.2
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15