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5059 Aluminum vs. S32750 Stainless Steel

5059 aluminum belongs to the aluminum alloys classification, while S32750 stainless steel belongs to the iron alloys. There are 31 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 5059 aluminum and the bottom bar is S32750 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
210
Elongation at Break, % 11 to 25
17
Fatigue Strength, MPa 170 to 240
360
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 26
81
Shear Strength, MPa 220 to 250
530
Tensile Strength: Ultimate (UTS), MPa 350 to 410
860
Tensile Strength: Yield (Proof), MPa 170 to 300
590

Thermal Properties

Latent Heat of Fusion, J/g 390
300
Maximum Temperature: Corrosion, °C 65
450
Maximum Temperature: Mechanical, °C 210
1100
Melting Completion (Liquidus), °C 650
1450
Melting Onset (Solidus), °C 510
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 24
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 95
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
21
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.1
4.1
Embodied Energy, MJ/kg 160
56
Embodied Water, L/kg 1160
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 75
130
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 650
860
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 36 to 42
31
Strength to Weight: Bending, points 41 to 45
26
Thermal Diffusivity, mm2/s 44
4.0
Thermal Shock Resistance, points 16 to 18
25

Alloy Composition


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Aluminum (Al), % 89.9 to 94
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.25
24 to 26
Copper (Cu), % 0 to 0.25
0 to 0.5
Iron (Fe), % 0 to 0.5
58.1 to 66.8
Magnesium (Mg), % 5.0 to 6.0
0
Manganese (Mn), % 0.6 to 1.2
0 to 1.2
Molybdenum (Mo), % 0
3.0 to 5.0
Nickel (Ni), % 0
6.0 to 8.0
Nitrogen (N), % 0
0.24 to 0.32
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.45
0 to 0.8
Sulfur (S), % 0
0 to 0.020
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