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6005A Aluminum vs. EN 1.7710 Steel

6005A aluminum belongs to the aluminum alloys classification, while EN 1.7710 steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 6005A aluminum and the bottom bar is EN 1.7710 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 8.6 to 17
6.8 to 11
Fatigue Strength, MPa 55 to 110
500 to 620
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Tensile Strength: Ultimate (UTS), MPa 190 to 300
930 to 1070
Tensile Strength: Yield (Proof), MPa 100 to 270
800 to 1060

Thermal Properties

Latent Heat of Fusion, J/g 410
260
Maximum Temperature: Mechanical, °C 170
440
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 600
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 180 to 190
41
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 47 to 50
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 150 to 170
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.2
Embodied Energy, MJ/kg 150
30
Embodied Water, L/kg 1180
57

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 29
73 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 76 to 530
1680 to 2970
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 20 to 30
33 to 38
Strength to Weight: Bending, points 27 to 36
27 to 30
Thermal Diffusivity, mm2/s 72 to 79
11
Thermal Shock Resistance, points 8.6 to 13
27 to 31

Alloy Composition

Aluminum (Al), % 96.5 to 99.1
0
Carbon (C), % 0
0.12 to 0.18
Chromium (Cr), % 0 to 0.3
1.3 to 1.8
Copper (Cu), % 0 to 0.3
0
Iron (Fe), % 0 to 0.35
95.1 to 97
Magnesium (Mg), % 0.4 to 0.7
0
Manganese (Mn), % 0 to 0.5
0.6 to 1.0
Molybdenum (Mo), % 0
0.8 to 1.0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0.5 to 0.9
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0
0.15 to 0.25
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants