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5383 Aluminum vs. EN 1.5410 Steel

5383 aluminum belongs to the aluminum alloys classification, while EN 1.5410 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 5383 aluminum and the bottom bar is EN 1.5410 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 110
170 to 190
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.7 to 15
20 to 25
Fatigue Strength, MPa 130 to 200
290 to 330
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Tensile Strength: Ultimate (UTS), MPa 310 to 370
560 to 620
Tensile Strength: Yield (Proof), MPa 150 to 310
400 to 480

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 200
400
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 540
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
51
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 97
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.3
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
1.7
Embodied Energy, MJ/kg 160
22
Embodied Water, L/kg 1170
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
120 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
430 to 610
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 32 to 38
20 to 22
Strength to Weight: Bending, points 38 to 42
19 to 21
Thermal Diffusivity, mm2/s 51
14
Thermal Shock Resistance, points 14 to 16
16 to 18

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0 to 0.12
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.25
96.9 to 98.6
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
1.2 to 1.8
Molybdenum (Mo), % 0
0.2 to 0.4
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.25
0 to 0.6
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.15
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0