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EN 1.4107 Stainless Steel vs. 5082 Aluminum

EN 1.4107 stainless steel belongs to the iron alloys classification, while 5082 aluminum belongs to the aluminum 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 EN 1.4107 stainless steel and the bottom bar is 5082 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
67
Elongation at Break, % 18 to 21
1.1
Fatigue Strength, MPa 260 to 350
110 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
25
Tensile Strength: Ultimate (UTS), MPa 620 to 700
380 to 400
Tensile Strength: Yield (Proof), MPa 400 to 570
300 to 340

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 740
180
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1410
560
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 27
130
Thermal Expansion, µm/m-K 10
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
32
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
110

Otherwise Unclassified Properties

Base Metal Price, % relative 7.5
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.1
8.9
Embodied Energy, MJ/kg 30
150
Embodied Water, L/kg 100
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 120
4.0 to 4.3
Resilience: Unit (Modulus of Resilience), kJ/m3 420 to 840
670 to 870
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 22 to 25
39 to 41
Strength to Weight: Bending, points 21 to 22
43 to 45
Thermal Diffusivity, mm2/s 7.2
54
Thermal Shock Resistance, points 22 to 25
17 to 18

Alloy Composition


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Aluminum (Al), % 0
93.5 to 96
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 11.5 to 12.5
0 to 0.15
Copper (Cu), % 0 to 0.3
0 to 0.15
Iron (Fe), % 83.8 to 87.2
0 to 0.35
Magnesium (Mg), % 0
4.0 to 5.0
Manganese (Mn), % 0.5 to 0.8
0 to 0.15
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 0.8 to 1.5
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.4
0 to 0.2
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.1
Vanadium (V), % 0 to 0.080
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants