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6016 Aluminum vs. AISI 440A Stainless Steel

6016 aluminum belongs to the aluminum alloys classification, while AISI 440A 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 6016 aluminum and the bottom bar is AISI 440A stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 11 to 27
5.0 to 20
Fatigue Strength, MPa 68 to 89
270 to 790
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 130 to 170
450 to 1040
Tensile Strength: Ultimate (UTS), MPa 200 to 280
730 to 1790
Tensile Strength: Yield (Proof), MPa 110 to 210
420 to 1650

Thermal Properties

Latent Heat of Fusion, J/g 410
280
Maximum Temperature: Mechanical, °C 160
760
Melting Completion (Liquidus), °C 660
1480
Melting Onset (Solidus), °C 610
1370
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 190 to 210
23
Thermal Expansion, µm/m-K 23
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 48 to 54
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 160 to 180
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.0
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.2
2.2
Embodied Energy, MJ/kg 150
31
Embodied Water, L/kg 1180
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 47
87 to 120
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 21 to 29
26 to 65
Strength to Weight: Bending, points 29 to 35
23 to 43
Thermal Diffusivity, mm2/s 77 to 86
6.2
Thermal Shock Resistance, points 9.1 to 12
26 to 65

Alloy Composition

Aluminum (Al), % 96.4 to 98.8
0
Carbon (C), % 0
0.6 to 0.75
Chromium (Cr), % 0 to 0.1
16 to 18
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.5
78.4 to 83.4
Magnesium (Mg), % 0.25 to 0.6
0
Manganese (Mn), % 0 to 0.2
0 to 1.0
Molybdenum (Mo), % 0
0 to 0.75
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 1.0 to 1.5
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0