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8090 Aluminum vs. EN 1.4567 Stainless Steel

8090 aluminum belongs to the aluminum alloys classification, while EN 1.4567 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (6, 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 EN 1.4567 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 3.5 to 13
22 to 51
Fatigue Strength, MPa 91 to 140
190 to 260
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
76
Tensile Strength: Ultimate (UTS), MPa 340 to 490
550 to 780
Tensile Strength: Yield (Proof), MPa 210 to 420
200 to 390

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 190
930
Melting Completion (Liquidus), °C 660
1410
Melting Onset (Solidus), °C 600
1370
Specific Heat Capacity, J/kg-K 960
480
Thermal Conductivity, W/m-K 95 to 160
11
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 20
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 66
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 18
16
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.6
3.1
Embodied Energy, MJ/kg 170
43
Embodied Water, L/kg 1160
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 41
150 to 220
Resilience: Unit (Modulus of Resilience), kJ/m3 340 to 1330
100 to 400
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 34 to 49
19 to 27
Strength to Weight: Bending, points 39 to 50
19 to 24
Thermal Diffusivity, mm2/s 36 to 60
3.0
Thermal Shock Resistance, points 15 to 22
12 to 17

Alloy Composition

Aluminum (Al), % 93 to 98.4
0
Carbon (C), % 0
0 to 0.040
Chromium (Cr), % 0 to 0.1
17 to 19
Copper (Cu), % 1.0 to 1.6
3.0 to 4.0
Iron (Fe), % 0 to 0.3
63.3 to 71.5
Lithium (Li), % 2.2 to 2.7
0
Magnesium (Mg), % 0.6 to 1.3
0
Manganese (Mn), % 0 to 0.1
0 to 2.0
Nickel (Ni), % 0
8.5 to 10.5
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.015
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