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5082 Aluminum vs. EN 1.7711 Steel

5082 aluminum belongs to the aluminum alloys classification, while EN 1.7711 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 5082 aluminum and the bottom bar is EN 1.7711 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 1.1
16 to 22
Fatigue Strength, MPa 110 to 130
290 to 520
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 25
73
Shear Strength, MPa 210 to 230
440 to 570
Tensile Strength: Ultimate (UTS), MPa 380 to 400
690 to 930
Tensile Strength: Yield (Proof), MPa 300 to 340
400 to 800

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 180
430
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 560
1420
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 130
33
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 110
8.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.0
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.9
2.3
Embodied Energy, MJ/kg 150
32
Embodied Water, L/kg 1180
54

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 4.3
130 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 670 to 870
430 to 1690
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 39 to 41
24 to 33
Strength to Weight: Bending, points 43 to 45
22 to 27
Thermal Diffusivity, mm2/s 54
8.9
Thermal Shock Resistance, points 17 to 18
24 to 32

Alloy Composition

Aluminum (Al), % 93.5 to 96
0 to 0.015
Carbon (C), % 0
0.36 to 0.44
Chromium (Cr), % 0 to 0.15
0.9 to 1.2
Copper (Cu), % 0 to 0.15
0
Iron (Fe), % 0 to 0.35
96 to 97.5
Magnesium (Mg), % 4.0 to 5.0
0
Manganese (Mn), % 0 to 0.15
0.45 to 0.85
Molybdenum (Mo), % 0
0.5 to 0.65
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.2
0 to 0.4
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0
0.25 to 0.35
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0