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5086 Aluminum vs. S42010 Stainless Steel

5086 aluminum belongs to the aluminum alloys classification, while S42010 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 5086 aluminum and the bottom bar is S42010 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.7 to 20
18
Fatigue Strength, MPa 88 to 180
220
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 160 to 230
370
Tensile Strength: Ultimate (UTS), MPa 270 to 390
590
Tensile Strength: Yield (Proof), MPa 110 to 320
350

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Corrosion, °C 65
390
Maximum Temperature: Mechanical, °C 190
800
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 590
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
29
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
2.7
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
8.5
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.8
2.2
Embodied Energy, MJ/kg 150
30
Embodied Water, L/kg 1180
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
95
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 28 to 40
21
Strength to Weight: Bending, points 34 to 44
20
Thermal Diffusivity, mm2/s 52
7.9
Thermal Shock Resistance, points 12 to 17
21

Alloy Composition

Aluminum (Al), % 93 to 96.3
0
Carbon (C), % 0
0.15 to 0.3
Chromium (Cr), % 0.050 to 0.25
13.5 to 15
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
80.9 to 85.6
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
0 to 1.0
Molybdenum (Mo), % 0
0.4 to 0.85
Nickel (Ni), % 0
0.35 to 0.85
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0