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7050 Aluminum vs. EN 1.4415 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.4415 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 1.4415 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
17 to 20
Fatigue Strength, MPa 130 to 210
470 to 510
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 280 to 330
520 to 570
Tensile Strength: Ultimate (UTS), MPa 490 to 570
830 to 930
Tensile Strength: Yield (Proof), MPa 390 to 500
730 to 840

Thermal Properties

Latent Heat of Fusion, J/g 370
280
Maximum Temperature: Mechanical, °C 190
790
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 490
1420
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 140
19
Thermal Expansion, µm/m-K 24
9.9

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 10
13
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.2
3.6
Embodied Energy, MJ/kg 150
51
Embodied Water, L/kg 1120
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
150 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
1350 to 1790
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
29 to 33
Strength to Weight: Bending, points 45 to 50
25 to 27
Thermal Diffusivity, mm2/s 54
5.1
Thermal Shock Resistance, points 21 to 25
30 to 34

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.040
11.5 to 13.5
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
75.9 to 82.4
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Molybdenum (Mo), % 0
1.5 to 2.5
Nickel (Ni), % 0
4.5 to 6.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.060
0 to 0.010
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0

Comparable Variants