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A390.0 Aluminum vs. S66286 Stainless Steel

A390.0 aluminum belongs to the aluminum alloys classification, while S66286 stainless steel belongs to the iron 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 A390.0 aluminum and the bottom bar is S66286 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 75
190
Elongation at Break, % 0.87 to 0.91
17 to 40
Fatigue Strength, MPa 70 to 100
240 to 410
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
75
Tensile Strength: Ultimate (UTS), MPa 190 to 290
620 to 1020
Tensile Strength: Yield (Proof), MPa 190 to 290
280 to 670

Thermal Properties

Latent Heat of Fusion, J/g 640
300
Maximum Temperature: Mechanical, °C 170
920
Melting Completion (Liquidus), °C 580
1430
Melting Onset (Solidus), °C 480
1370
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 20
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 20
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 67
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 11
26
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 7.3
6.0
Embodied Energy, MJ/kg 140
87
Embodied Water, L/kg 950
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.6 to 2.6
150 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 240 to 580
190 to 1150
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 52
24
Strength to Weight: Axial, points 19 to 30
22 to 36
Strength to Weight: Bending, points 27 to 36
20 to 28
Thermal Diffusivity, mm2/s 56
4.0
Thermal Shock Resistance, points 9.0 to 14
13 to 22

Alloy Composition

Aluminum (Al), % 75.3 to 79.6
0 to 0.35
Boron (B), % 0
0.0010 to 0.010
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
13.5 to 16
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 0.5
49.1 to 59.5
Magnesium (Mg), % 0.45 to 0.65
0
Manganese (Mn), % 0 to 0.1
0 to 2.0
Molybdenum (Mo), % 0
1.0 to 1.5
Nickel (Ni), % 0
24 to 27
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 16 to 18
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
1.9 to 2.4
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.2
0