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7050 Aluminum vs. S44660 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while S44660 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 S44660 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 2.2 to 12
20
Fatigue Strength, MPa 130 to 210
330
Poisson's Ratio 0.32
0.27
Shear Modulus, GPa 26
81
Shear Strength, MPa 280 to 330
410
Tensile Strength: Ultimate (UTS), MPa 490 to 570
660
Tensile Strength: Yield (Proof), MPa 390 to 500
510

Thermal Properties

Latent Heat of Fusion, J/g 370
300
Maximum Temperature: Mechanical, °C 190
1100
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 490
1410
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 140
17
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 10
21
Density, g/cm3 3.1
7.7
Embodied Carbon, kg CO2/kg material 8.2
4.3
Embodied Energy, MJ/kg 150
61
Embodied Water, L/kg 1120
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
120
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
640
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
24
Strength to Weight: Bending, points 45 to 50
22
Thermal Diffusivity, mm2/s 54
4.5
Thermal Shock Resistance, points 21 to 25
21

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.040
25 to 28
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
60.4 to 71
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Molybdenum (Mo), % 0
3.0 to 4.0
Nickel (Ni), % 0
1.0 to 3.5
Niobium (Nb), % 0
0.2 to 1.0
Nitrogen (N), % 0
0 to 0.040
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.12
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0.2 to 1.0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0