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S66286 Stainless Steel vs. 8090 Aluminum

S66286 stainless steel belongs to the iron alloys classification, while 8090 aluminum belongs to the aluminum alloys. There are 29 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 S66286 stainless steel and the bottom bar is 8090 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
67
Elongation at Break, % 17 to 40
3.5 to 13
Fatigue Strength, MPa 240 to 410
91 to 140
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
25
Tensile Strength: Ultimate (UTS), MPa 620 to 1020
340 to 490
Tensile Strength: Yield (Proof), MPa 280 to 670
210 to 420

Thermal Properties

Latent Heat of Fusion, J/g 300
400
Maximum Temperature: Mechanical, °C 920
190
Melting Completion (Liquidus), °C 1430
660
Melting Onset (Solidus), °C 1370
600
Specific Heat Capacity, J/kg-K 470
960
Thermal Conductivity, W/m-K 15
95 to 160
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
20
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
66

Otherwise Unclassified Properties

Base Metal Price, % relative 26
18
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 6.0
8.6
Embodied Energy, MJ/kg 87
170
Embodied Water, L/kg 170
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 200
16 to 41
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 1150
340 to 1330
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 22 to 36
34 to 49
Strength to Weight: Bending, points 20 to 28
39 to 50
Thermal Diffusivity, mm2/s 4.0
36 to 60
Thermal Shock Resistance, points 13 to 22
15 to 22

Alloy Composition

Aluminum (Al), % 0 to 0.35
93 to 98.4
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13.5 to 16
0 to 0.1
Copper (Cu), % 0
1.0 to 1.6
Iron (Fe), % 49.1 to 59.5
0 to 0.3
Lithium (Li), % 0
2.2 to 2.7
Magnesium (Mg), % 0
0.6 to 1.3
Manganese (Mn), % 0 to 2.0
0 to 0.1
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 1.9 to 2.4
0 to 0.1
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0
0.040 to 0.16
Residuals, % 0
0 to 0.15