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6110A Aluminum vs. EN 1.1132 Steel

6110A aluminum belongs to the aluminum alloys classification, while EN 1.1132 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 6110A aluminum and the bottom bar is EN 1.1132 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 11 to 18
12 to 24
Fatigue Strength, MPa 140 to 210
180 to 280
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 220 to 280
260 to 310
Tensile Strength: Ultimate (UTS), MPa 360 to 470
370 to 490
Tensile Strength: Yield (Proof), MPa 250 to 430
240 to 400

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 190
400
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 600
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 160
51
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
7.0
Electrical Conductivity: Equal Weight (Specific), % IACS 140
8.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.8
Density, g/cm3 2.8
7.9
Embodied Carbon, kg CO2/kg material 8.4
1.4
Embodied Energy, MJ/kg 150
18
Embodied Water, L/kg 1170
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 47 to 58
38 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 1300
160 to 430
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 36 to 47
13 to 17
Strength to Weight: Bending, points 41 to 48
15 to 18
Thermal Diffusivity, mm2/s 65
14
Thermal Shock Resistance, points 16 to 21
12 to 16

Alloy Composition

Aluminum (Al), % 94.8 to 98
0
Carbon (C), % 0
0.13 to 0.17
Chromium (Cr), % 0.050 to 0.25
0
Copper (Cu), % 0.3 to 0.8
0 to 0.25
Iron (Fe), % 0 to 0.5
98.6 to 99.57
Magnesium (Mg), % 0.7 to 1.1
0
Manganese (Mn), % 0.3 to 0.9
0.3 to 0.6
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0.7 to 1.1
0 to 0.3
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0