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7050 Aluminum vs. EN 1.4313 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.4313 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 1.4313 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
12 to 17
Fatigue Strength, MPa 130 to 210
340 to 510
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 280 to 330
460 to 600
Tensile Strength: Ultimate (UTS), MPa 490 to 570
750 to 1000
Tensile Strength: Yield (Proof), MPa 390 to 500
580 to 910

Thermal Properties

Latent Heat of Fusion, J/g 370
280
Maximum Temperature: Mechanical, °C 190
780
Melting Completion (Liquidus), °C 630
1450
Melting Onset (Solidus), °C 490
1400
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 140
25
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
10
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.4
Embodied Energy, MJ/kg 150
34
Embodied Water, L/kg 1120
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
870 to 2100
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
27 to 36
Strength to Weight: Bending, points 45 to 50
23 to 28
Thermal Diffusivity, mm2/s 54
6.7
Thermal Shock Resistance, points 21 to 25
27 to 36

Alloy Composition


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Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.040
12 to 14
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
78.5 to 84.2
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.5
Molybdenum (Mo), % 0
0.3 to 0.7
Nickel (Ni), % 0
3.5 to 4.5
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.12
0 to 0.7
Sulfur (S), % 0
0 to 0.015
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