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7050 Aluminum vs. EN 1.4938 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.4938 stainless steel belongs to the iron 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 7050 aluminum and the bottom bar is EN 1.4938 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
16 to 17
Fatigue Strength, MPa 130 to 210
390 to 520
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 280 to 330
540 to 630
Tensile Strength: Ultimate (UTS), MPa 490 to 570
870 to 1030
Tensile Strength: Yield (Proof), MPa 390 to 500
640 to 870

Thermal Properties

Latent Heat of Fusion, J/g 370
270
Maximum Temperature: Mechanical, °C 190
750
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
30
Thermal Expansion, µm/m-K 24
11

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
3.3
Embodied Energy, MJ/kg 150
47
Embodied Water, L/kg 1120
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
140 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
1050 to 1920
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
31 to 37
Strength to Weight: Bending, points 45 to 50
26 to 29
Thermal Diffusivity, mm2/s 54
8.1
Thermal Shock Resistance, points 21 to 25
30 to 35

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0 to 0.040
11 to 12.5
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
80.5 to 84.8
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0.4 to 0.9
Molybdenum (Mo), % 0
1.5 to 2.0
Nickel (Ni), % 0
2.0 to 3.0
Nitrogen (N), % 0
0.020 to 0.040
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.060
0
Vanadium (V), % 0
0.25 to 0.4
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0