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8090 Aluminum vs. S36200 Stainless Steel

8090 aluminum belongs to the aluminum alloys classification, while S36200 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 S36200 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 3.5 to 13
3.4 to 4.6
Fatigue Strength, MPa 91 to 140
450 to 570
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
76
Tensile Strength: Ultimate (UTS), MPa 340 to 490
1180 to 1410
Tensile Strength: Yield (Proof), MPa 210 to 420
960 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 190
820
Melting Completion (Liquidus), °C 660
1440
Melting Onset (Solidus), °C 600
1400
Specific Heat Capacity, J/kg-K 960
480
Thermal Conductivity, W/m-K 95 to 160
16
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 20
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 66
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 18
12
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.6
2.8
Embodied Energy, MJ/kg 170
40
Embodied Water, L/kg 1160
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 41
46 to 51
Resilience: Unit (Modulus of Resilience), kJ/m3 340 to 1330
2380 to 3930
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 34 to 49
42 to 50
Strength to Weight: Bending, points 39 to 50
32 to 36
Thermal Diffusivity, mm2/s 36 to 60
4.3
Thermal Shock Resistance, points 15 to 22
40 to 48

Alloy Composition

Aluminum (Al), % 93 to 98.4
0 to 0.1
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.1
14 to 14.5
Copper (Cu), % 1.0 to 1.6
0
Iron (Fe), % 0 to 0.3
75.4 to 79.5
Lithium (Li), % 2.2 to 2.7
0
Magnesium (Mg), % 0.6 to 1.3
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Molybdenum (Mo), % 0
0 to 0.3
Nickel (Ni), % 0
6.5 to 7.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.2
0 to 0.3
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0.6 to 0.9
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0.040 to 0.16
0
Residuals, % 0 to 0.15
0