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8090 Aluminum vs. S35500 Stainless Steel

8090 aluminum belongs to the aluminum alloys classification, while S35500 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 8090 aluminum and the bottom bar is S35500 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
200
Elongation at Break, % 3.5 to 13
14
Fatigue Strength, MPa 91 to 140
690 to 730
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
78
Tensile Strength: Ultimate (UTS), MPa 340 to 490
1330 to 1490
Tensile Strength: Yield (Proof), MPa 210 to 420
1200 to 1280

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 190
870
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 600
1420
Specific Heat Capacity, J/kg-K 960
470
Thermal Conductivity, W/m-K 95 to 160
16
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 20
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 66
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 18
16
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.6
3.5
Embodied Energy, MJ/kg 170
47
Embodied Water, L/kg 1160
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 41
180 to 190
Resilience: Unit (Modulus of Resilience), kJ/m3 340 to 1330
3610 to 4100
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 34 to 49
47 to 53
Strength to Weight: Bending, points 39 to 50
34 to 37
Thermal Diffusivity, mm2/s 36 to 60
4.4
Thermal Shock Resistance, points 15 to 22
44 to 49

Alloy Composition


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Aluminum (Al), % 93 to 98.4
0
Carbon (C), % 0
0.1 to 0.15
Chromium (Cr), % 0 to 0.1
15 to 16
Copper (Cu), % 1.0 to 1.6
0
Iron (Fe), % 0 to 0.3
73.2 to 77.7
Lithium (Li), % 2.2 to 2.7
0
Magnesium (Mg), % 0.6 to 1.3
0
Manganese (Mn), % 0 to 0.1
0.5 to 1.3
Molybdenum (Mo), % 0
2.5 to 3.2
Nickel (Ni), % 0
4.0 to 5.0
Niobium (Nb), % 0
0.1 to 0.5
Nitrogen (N), % 0
0.070 to 0.13
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0.040 to 0.16
0
Residuals, % 0 to 0.15
0

Comparable Variants