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7005 Aluminum vs. EN 1.6553 Steel

7005 aluminum belongs to the aluminum alloys classification, while EN 1.6553 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 7005 aluminum and the bottom bar is EN 1.6553 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 10 to 20
19 to 21
Fatigue Strength, MPa 100 to 190
330 to 460
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Tensile Strength: Ultimate (UTS), MPa 200 to 400
710 to 800
Tensile Strength: Yield (Proof), MPa 95 to 350
470 to 670

Thermal Properties

Latent Heat of Fusion, J/g 380
250
Maximum Temperature: Mechanical, °C 200
420
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 610
1420
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 140 to 170
39
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 43
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 110 to 130
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.7
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.6
Embodied Energy, MJ/kg 150
21
Embodied Water, L/kg 1150
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
130 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
600 to 1190
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 19 to 38
25 to 28
Strength to Weight: Bending, points 26 to 41
23 to 24
Thermal Diffusivity, mm2/s 54 to 65
10
Thermal Shock Resistance, points 8.7 to 18
21 to 23

Alloy Composition

Aluminum (Al), % 91 to 94.7
0
Carbon (C), % 0
0.23 to 0.28
Chromium (Cr), % 0.060 to 0.2
0.4 to 0.8
Copper (Cu), % 0 to 0.1
0 to 0.3
Iron (Fe), % 0 to 0.4
95.6 to 98.2
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0.6 to 1.0
Molybdenum (Mo), % 0
0.15 to 0.3
Nickel (Ni), % 0
0.4 to 0.8
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.35
0 to 0.8
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0.010 to 0.060
0
Vanadium (V), % 0
0 to 0.030
Zinc (Zn), % 4.0 to 5.0
0
Zirconium (Zr), % 0.080 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants