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7050 Aluminum vs. EN 1.4618 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.4618 stainless steel belongs to the iron alloys. There are 30 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 1.4618 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
51
Fatigue Strength, MPa 130 to 210
240 to 250
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 280 to 330
480 to 500
Tensile Strength: Ultimate (UTS), MPa 490 to 570
680 to 700
Tensile Strength: Yield (Proof), MPa 390 to 500
250 to 260

Thermal Properties

Latent Heat of Fusion, J/g 370
280
Maximum Temperature: Mechanical, °C 190
900
Melting Completion (Liquidus), °C 630
1400
Melting Onset (Solidus), °C 490
1360
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 140
15
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
13
Density, g/cm3 3.1
7.7
Embodied Carbon, kg CO2/kg material 8.2
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1120
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
270 to 280
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
160 to 170
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
24 to 25
Strength to Weight: Bending, points 45 to 50
22 to 23
Thermal Diffusivity, mm2/s 54
4.0
Thermal Shock Resistance, points 21 to 25
15 to 16

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.040
16.5 to 18.5
Copper (Cu), % 2.0 to 2.6
1.0 to 2.5
Iron (Fe), % 0 to 0.15
62.7 to 72.5
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
5.5 to 9.5
Nickel (Ni), % 0
4.5 to 5.5
Nitrogen (N), % 0
0 to 0.15
Phosphorus (P), % 0
0 to 0.070
Silicon (Si), % 0 to 0.12
0 to 1.0
Sulfur (S), % 0
0 to 0.010
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