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5059 Aluminum vs. S32053 Stainless Steel

5059 aluminum belongs to the aluminum alloys classification, while S32053 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 S32053 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
210
Elongation at Break, % 11 to 25
46
Fatigue Strength, MPa 170 to 240
310
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
80
Shear Strength, MPa 220 to 250
510
Tensile Strength: Ultimate (UTS), MPa 350 to 410
730
Tensile Strength: Yield (Proof), MPa 170 to 300
330

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Corrosion, °C 65
440
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
470
Thermal Conductivity, W/m-K 110
13
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 95
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
33
Density, g/cm3 2.7
8.1
Embodied Carbon, kg CO2/kg material 9.1
6.1
Embodied Energy, MJ/kg 160
83
Embodied Water, L/kg 1160
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 75
270
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 650
270
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 36 to 42
25
Strength to Weight: Bending, points 41 to 45
22
Thermal Diffusivity, mm2/s 44
3.3
Thermal Shock Resistance, points 16 to 18
16

Alloy Composition

Aluminum (Al), % 89.9 to 94
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.25
22 to 24
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.5
41.7 to 48.8
Magnesium (Mg), % 5.0 to 6.0
0
Manganese (Mn), % 0.6 to 1.2
0 to 1.0
Molybdenum (Mo), % 0
5.0 to 6.0
Nickel (Ni), % 0
24 to 26
Nitrogen (N), % 0
0.17 to 0.22
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.45
0 to 1.0
Sulfur (S), % 0
0 to 0.010
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