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6182 Aluminum vs. EN 1.5535 Steel

6182 aluminum belongs to the aluminum alloys classification, while EN 1.5535 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 6182 aluminum and the bottom bar is EN 1.5535 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 6.8 to 13
11 to 22
Fatigue Strength, MPa 63 to 99
210 to 320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 140 to 190
320 to 370
Tensile Strength: Ultimate (UTS), MPa 230 to 320
450 to 1490
Tensile Strength: Yield (Proof), MPa 130 to 270
300 to 500

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 190
400
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 600
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 160
50
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.9
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.4
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1170
48

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21 to 26
45 to 250
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 520
240 to 680
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 23 to 32
16 to 53
Strength to Weight: Bending, points 30 to 38
17 to 37
Thermal Diffusivity, mm2/s 65
13
Thermal Shock Resistance, points 10 to 14
13 to 44

Alloy Composition

Aluminum (Al), % 95 to 97.9
0
Boron (B), % 0
0.00080 to 0.0050
Carbon (C), % 0
0.2 to 0.25
Chromium (Cr), % 0 to 0.25
0 to 0.3
Copper (Cu), % 0 to 0.1
0 to 0.25
Iron (Fe), % 0 to 0.5
97.6 to 98.9
Magnesium (Mg), % 0.7 to 1.2
0
Manganese (Mn), % 0.5 to 1.0
0.9 to 1.2
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0.9 to 1.3
0 to 0.3
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.050 to 0.2
0
Residuals, % 0 to 0.15
0