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S17400 Stainless Steel vs. 8090 Aluminum

S17400 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 (8, 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 S17400 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, % 11 to 21
3.5 to 13
Fatigue Strength, MPa 380 to 670
91 to 140
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
25
Tensile Strength: Ultimate (UTS), MPa 910 to 1390
340 to 490
Tensile Strength: Yield (Proof), MPa 580 to 1250
210 to 420

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 850
190
Melting Completion (Liquidus), °C 1440
660
Melting Onset (Solidus), °C 1400
600
Specific Heat Capacity, J/kg-K 480
960
Thermal Conductivity, W/m-K 17
95 to 160
Thermal Expansion, µm/m-K 11
24

Electrical Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 14
18
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.6
Embodied Energy, MJ/kg 39
170
Embodied Water, L/kg 130
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 160
16 to 41
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4060
340 to 1330
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 32 to 49
34 to 49
Strength to Weight: Bending, points 27 to 35
39 to 50
Thermal Diffusivity, mm2/s 4.5
36 to 60
Thermal Shock Resistance, points 30 to 46
15 to 22

Alloy Composition

Aluminum (Al), % 0
93 to 98.4
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0 to 0.1
Copper (Cu), % 3.0 to 5.0
1.0 to 1.6
Iron (Fe), % 70.4 to 78.9
0 to 0.3
Lithium (Li), % 0
2.2 to 2.7
Magnesium (Mg), % 0
0.6 to 1.3
Manganese (Mn), % 0 to 1.0
0 to 0.1
Nickel (Ni), % 3.0 to 5.0
0
Niobium (Nb), % 0.15 to 0.45
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), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0
0.040 to 0.16
Residuals, % 0
0 to 0.15