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5059 Aluminum vs. S20161 Stainless Steel

5059 aluminum belongs to the aluminum alloys classification, while S20161 stainless steel belongs to the iron alloys. There are 31 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 5059 aluminum and the bottom bar is S20161 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 11 to 25
46
Fatigue Strength, MPa 170 to 240
360
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 220 to 250
690
Tensile Strength: Ultimate (UTS), MPa 350 to 410
980
Tensile Strength: Yield (Proof), MPa 170 to 300
390

Thermal Properties

Latent Heat of Fusion, J/g 390
330
Maximum Temperature: Corrosion, °C 65
410
Maximum Temperature: Mechanical, °C 210
870
Melting Completion (Liquidus), °C 650
1380
Melting Onset (Solidus), °C 510
1330
Specific Heat Capacity, J/kg-K 900
490
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 95
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
7.5
Embodied Carbon, kg CO2/kg material 9.1
2.7
Embodied Energy, MJ/kg 160
39
Embodied Water, L/kg 1160
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 75
360
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 650
390
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
26
Strength to Weight: Axial, points 36 to 42
36
Strength to Weight: Bending, points 41 to 45
29
Thermal Diffusivity, mm2/s 44
4.0
Thermal Shock Resistance, points 16 to 18
22

Alloy Composition


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Aluminum (Al), % 89.9 to 94
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0 to 0.25
15 to 18
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.5
65.6 to 73.9
Magnesium (Mg), % 5.0 to 6.0
0
Manganese (Mn), % 0.6 to 1.2
4.0 to 6.0
Nickel (Ni), % 0
4.0 to 6.0
Nitrogen (N), % 0
0.080 to 0.2
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.45
3.0 to 4.0
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0.4 to 0.9
0
Zirconium (Zr), % 0.050 to 0.25
0
Residuals, % 0 to 0.15
0