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EN 1.4409 Stainless Steel vs. 6016 Aluminum

EN 1.4409 stainless steel belongs to the iron alloys classification, while 6016 aluminum belongs to the aluminum alloys. There are 30 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 EN 1.4409 stainless steel and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140
55 to 80
Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 34
11 to 27
Fatigue Strength, MPa 180
68 to 89
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
26
Tensile Strength: Ultimate (UTS), MPa 490
200 to 280
Tensile Strength: Yield (Proof), MPa 220
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Maximum Temperature: Mechanical, °C 990
160
Melting Completion (Liquidus), °C 1440
660
Melting Onset (Solidus), °C 1390
610
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 15
190 to 210
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.1
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 19
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.7
8.2
Embodied Energy, MJ/kg 52
150
Embodied Water, L/kg 160
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 120
82 to 340
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 17
21 to 29
Strength to Weight: Bending, points 18
29 to 35
Thermal Diffusivity, mm2/s 4.1
77 to 86
Thermal Shock Resistance, points 11
9.1 to 12

Alloy Composition

Aluminum (Al), % 0
96.4 to 98.8
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 18 to 20
0 to 0.1
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 61.7 to 71
0 to 0.5
Magnesium (Mg), % 0
0.25 to 0.6
Manganese (Mn), % 0 to 2.0
0 to 0.2
Molybdenum (Mo), % 2.0 to 2.5
0
Nickel (Ni), % 9.0 to 12
0
Nitrogen (N), % 0 to 0.2
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.5
1.0 to 1.5
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15