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7050 Aluminum vs. EN 1.4421 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.4421 stainless steel belongs to the iron alloys. There are 29 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 7050 aluminum and the bottom bar is EN 1.4421 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
11 to 17
Fatigue Strength, MPa 130 to 210
380 to 520
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
77
Tensile Strength: Ultimate (UTS), MPa 490 to 570
880 to 1100
Tensile Strength: Yield (Proof), MPa 390 to 500
620 to 950

Thermal Properties

Latent Heat of Fusion, J/g 370
280
Maximum Temperature: Mechanical, °C 190
870
Melting Completion (Liquidus), °C 630
1440
Melting Onset (Solidus), °C 490
1400
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 140
16
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
12
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.6
Embodied Energy, MJ/kg 150
36
Embodied Water, L/kg 1120
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
120 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
960 to 2270
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
31 to 39
Strength to Weight: Bending, points 45 to 50
26 to 30
Thermal Diffusivity, mm2/s 54
4.4
Thermal Shock Resistance, points 21 to 25
31 to 39

Alloy Composition


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Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.060
Chromium (Cr), % 0 to 0.040
15.5 to 17.5
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
74.4 to 80.5
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Molybdenum (Mo), % 0
0 to 0.7
Nickel (Ni), % 0
4.0 to 5.5
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.12
0 to 0.8
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0

Comparable Variants