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6008 Aluminum vs. EN 1.0213 Steel

6008 aluminum belongs to the aluminum alloys classification, while EN 1.0213 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 6008 aluminum and the bottom bar is EN 1.0213 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 9.1 to 17
12 to 25
Fatigue Strength, MPa 55 to 88
160 to 240
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 120 to 170
230 to 270
Tensile Strength: Ultimate (UTS), MPa 200 to 290
320 to 430
Tensile Strength: Yield (Proof), MPa 100 to 220
220 to 330

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 180
400
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 620
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 190
53
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49
6.9
Electrical Conductivity: Equal Weight (Specific), % IACS 160
7.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.8
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.5
1.4
Embodied Energy, MJ/kg 160
18
Embodied Water, L/kg 1180
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 28
33 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 76 to 360
120 to 300
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 21 to 29
11 to 15
Strength to Weight: Bending, points 28 to 35
13 to 16
Thermal Diffusivity, mm2/s 77
14
Thermal Shock Resistance, points 9.0 to 13
10 to 14

Alloy Composition

Aluminum (Al), % 96.5 to 99.1
0.020 to 0.060
Carbon (C), % 0
0.060 to 0.1
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.3
0
Iron (Fe), % 0 to 0.35
99.245 to 99.67
Magnesium (Mg), % 0.4 to 0.7
0
Manganese (Mn), % 0 to 0.3
0.25 to 0.45
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.5 to 0.9
0 to 0.1
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0.050 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0