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EN 1.5113 Steel vs. 6162 Aluminum

EN 1.5113 steel belongs to the iron alloys classification, while 6162 aluminum belongs to the aluminum alloys. There are 30 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 EN 1.5113 steel and the bottom bar is 6162 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 11 to 18
6.7 to 9.1
Fatigue Strength, MPa 220 to 470
100 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 360 to 540
170 to 180
Tensile Strength: Ultimate (UTS), MPa 580 to 900
290 to 300
Tensile Strength: Yield (Proof), MPa 320 to 770
260 to 270

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 400
160
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1410
620
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 52
190
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
50
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
170

Otherwise Unclassified Properties

Base Metal Price, % relative 2.0
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.4
8.3
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 48
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 91 to 96
19 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 270 to 1570
510 to 550
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 21 to 32
29 to 30
Strength to Weight: Bending, points 20 to 27
36
Thermal Diffusivity, mm2/s 14
79
Thermal Shock Resistance, points 17 to 26
13

Alloy Composition

Aluminum (Al), % 0
96.7 to 98.9
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 97 to 97.5
0 to 0.5
Magnesium (Mg), % 0
0.7 to 1.1
Manganese (Mn), % 1.6 to 1.8
0 to 0.1
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.9 to 1.1
0.4 to 0.8
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15