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EN 1.4474 Stainless Steel vs. 5086 Aluminum

EN 1.4474 stainless steel belongs to the iron alloys classification, while 5086 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 1.4474 stainless steel and the bottom bar is 5086 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 23
1.7 to 20
Fatigue Strength, MPa 320
88 to 180
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 80
26
Tensile Strength: Ultimate (UTS), MPa 670
270 to 390
Tensile Strength: Yield (Proof), MPa 480
110 to 320

Thermal Properties

Latent Heat of Fusion, J/g 300
400
Maximum Temperature: Corrosion, °C 450
65
Maximum Temperature: Mechanical, °C 1100
190
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1390
590
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 17
130
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.1
31
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
100

Otherwise Unclassified Properties

Base Metal Price, % relative 17
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 3.4
8.8
Embodied Energy, MJ/kg 48
150
Embodied Water, L/kg 170
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
5.8 to 42
Resilience: Unit (Modulus of Resilience), kJ/m3 560
86 to 770
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 24
28 to 40
Strength to Weight: Bending, points 22
34 to 44
Thermal Diffusivity, mm2/s 4.6
52
Thermal Shock Resistance, points 18
12 to 17

Alloy Composition

Aluminum (Al), % 0
93 to 96.3
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 25 to 27
0.050 to 0.25
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 61.2 to 69.1
0 to 0.5
Magnesium (Mg), % 0
3.5 to 4.5
Manganese (Mn), % 0 to 2.0
0.2 to 0.7
Molybdenum (Mo), % 1.3 to 2.0
0
Nickel (Ni), % 4.5 to 6.5
0
Nitrogen (N), % 0.12 to 0.2
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15