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8090 Aluminum vs. S21904 Stainless Steel

8090 aluminum belongs to the aluminum alloys classification, while S21904 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 S21904 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
200
Elongation at Break, % 3.5 to 13
17 to 51
Fatigue Strength, MPa 91 to 140
380 to 550
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
78
Tensile Strength: Ultimate (UTS), MPa 340 to 490
700 to 1000
Tensile Strength: Yield (Proof), MPa 210 to 420
390 to 910

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 190
980
Melting Completion (Liquidus), °C 660
1400
Melting Onset (Solidus), °C 600
1350
Specific Heat Capacity, J/kg-K 960
480
Thermal Conductivity, W/m-K 95 to 160
14
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 20
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 66
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 18
15
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.6
3.0
Embodied Energy, MJ/kg 170
43
Embodied Water, L/kg 1160
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 41
160 to 310
Resilience: Unit (Modulus of Resilience), kJ/m3 340 to 1330
380 to 2070
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 34 to 49
25 to 36
Strength to Weight: Bending, points 39 to 50
23 to 29
Thermal Diffusivity, mm2/s 36 to 60
3.8
Thermal Shock Resistance, points 15 to 22
15 to 21

Alloy Composition

Aluminum (Al), % 93 to 98.4
0
Carbon (C), % 0
0 to 0.040
Chromium (Cr), % 0 to 0.1
19 to 21.5
Copper (Cu), % 1.0 to 1.6
0
Iron (Fe), % 0 to 0.3
59.5 to 67.4
Lithium (Li), % 2.2 to 2.7
0
Magnesium (Mg), % 0.6 to 1.3
0
Manganese (Mn), % 0 to 0.1
8.0 to 10
Nickel (Ni), % 0
5.5 to 7.5
Nitrogen (N), % 0
0.15 to 0.4
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.2
0 to 1.0
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