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5383 Aluminum vs. S82012 Stainless Steel

5383 aluminum belongs to the aluminum alloys classification, while S82012 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 5383 aluminum and the bottom bar is S82012 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 6.7 to 15
40
Fatigue Strength, MPa 130 to 200
480
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 190 to 220
550
Tensile Strength: Ultimate (UTS), MPa 310 to 370
800
Tensile Strength: Yield (Proof), MPa 150 to 310
560

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Corrosion, °C 65
420
Maximum Temperature: Mechanical, °C 200
950
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 540
1380
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 97
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 9.0
2.4
Embodied Energy, MJ/kg 160
35
Embodied Water, L/kg 1170
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
290
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
790
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 32 to 38
29
Strength to Weight: Bending, points 38 to 42
25
Thermal Diffusivity, mm2/s 51
3.9
Thermal Shock Resistance, points 14 to 16
23

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.25
19 to 20.5
Copper (Cu), % 0 to 0.2
0 to 1.0
Iron (Fe), % 0 to 0.25
71.3 to 77.9
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
2.0 to 4.0
Molybdenum (Mo), % 0
0.1 to 0.6
Nickel (Ni), % 0
0.8 to 1.5
Nitrogen (N), % 0
0.16 to 0.26
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.25
0 to 0.8
Sulfur (S), % 0
0 to 0.0050
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0