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EN 1.4107 Stainless Steel vs. 7020 Aluminum

EN 1.4107 stainless steel belongs to the iron alloys classification, while 7020 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 1.4107 stainless steel and the bottom bar is 7020 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 18 to 21
8.4 to 14
Fatigue Strength, MPa 260 to 350
110 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Tensile Strength: Ultimate (UTS), MPa 620 to 700
190 to 390
Tensile Strength: Yield (Proof), MPa 400 to 570
120 to 310

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Maximum Temperature: Mechanical, °C 740
210
Melting Completion (Liquidus), °C 1450
650
Melting Onset (Solidus), °C 1410
610
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 27
150
Thermal Expansion, µm/m-K 10
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
39
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
120

Otherwise Unclassified Properties

Base Metal Price, % relative 7.5
9.5
Density, g/cm3 7.8
2.9
Embodied Carbon, kg CO2/kg material 2.1
8.3
Embodied Energy, MJ/kg 30
150
Embodied Water, L/kg 100
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 120
23 to 46
Resilience: Unit (Modulus of Resilience), kJ/m3 420 to 840
110 to 690
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 22 to 25
18 to 37
Strength to Weight: Bending, points 21 to 22
25 to 41
Thermal Diffusivity, mm2/s 7.2
59
Thermal Shock Resistance, points 22 to 25
8.3 to 17

Alloy Composition


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Aluminum (Al), % 0
91.2 to 94.8
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 11.5 to 12.5
0.1 to 0.35
Copper (Cu), % 0 to 0.3
0 to 0.2
Iron (Fe), % 83.8 to 87.2
0 to 0.4
Magnesium (Mg), % 0
1.0 to 1.4
Manganese (Mn), % 0.5 to 0.8
0.050 to 0.5
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 0.8 to 1.5
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.4
0 to 0.35
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.25
Vanadium (V), % 0 to 0.080
0
Zinc (Zn), % 0
4.0 to 5.0
Zirconium (Zr), % 0
0.080 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants