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5457 Aluminum vs. EN 1.6580 Steel

5457 aluminum belongs to the aluminum alloys classification, while EN 1.6580 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 5457 aluminum and the bottom bar is EN 1.6580 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 32 to 55
220 to 350
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.0 to 22
11 to 19
Fatigue Strength, MPa 55 to 98
310 to 610
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 85 to 130
450 to 700
Tensile Strength: Ultimate (UTS), MPa 130 to 210
720 to 1170
Tensile Strength: Yield (Proof), MPa 50 to 190
460 to 990

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 180
450
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 630
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 180
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 46
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 150
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.3
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.4
1.8
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 1190
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 23
120 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 250
560 to 2590
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 13 to 21
26 to 41
Strength to Weight: Bending, points 21 to 28
23 to 31
Thermal Diffusivity, mm2/s 72
11
Thermal Shock Resistance, points 5.7 to 9.0
21 to 34

Alloy Composition

Aluminum (Al), % 97.8 to 99.05
0
Carbon (C), % 0
0.26 to 0.34
Chromium (Cr), % 0
1.8 to 2.2
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.1
93.7 to 95.5
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0.15 to 0.45
0.3 to 0.6
Molybdenum (Mo), % 0
0.3 to 0.5
Nickel (Ni), % 0
1.8 to 2.2
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.080
0 to 0.4
Sulfur (S), % 0
0 to 0.035
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0

Comparable Variants