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7050 Aluminum vs. EN 1.7767 Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.7767 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 7050 aluminum and the bottom bar is EN 1.7767 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2 to 12
20
Fatigue Strength, MPa 130 to 210
320 to 340
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 280 to 330
420 to 430
Tensile Strength: Ultimate (UTS), MPa 490 to 570
670 to 690
Tensile Strength: Yield (Proof), MPa 390 to 500
460 to 500

Thermal Properties

Latent Heat of Fusion, J/g 370
250
Maximum Temperature: Mechanical, °C 190
480
Melting Completion (Liquidus), °C 630
1470
Melting Onset (Solidus), °C 490
1430
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 140
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 10
4.5
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.2
2.4
Embodied Energy, MJ/kg 150
33
Embodied Water, L/kg 1120
64

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
120 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
570 to 650
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 45 to 51
24
Strength to Weight: Bending, points 45 to 50
22
Thermal Diffusivity, mm2/s 54
11
Thermal Shock Resistance, points 21 to 25
19 to 20

Alloy Composition


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Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0.1 to 0.15
Chromium (Cr), % 0 to 0.040
2.8 to 3.3
Copper (Cu), % 2.0 to 2.6
0 to 0.25
Iron (Fe), % 0 to 0.15
93.8 to 95.8
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0 to 0.25
Niobium (Nb), % 0
0 to 0.070
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.12
0 to 0.15
Sulfur (S), % 0
0 to 0.0050
Titanium (Ti), % 0 to 0.060
0 to 0.030
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0