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7050 Aluminum vs. ASTM A182 Grade F5a

7050 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F5a 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 ASTM A182 grade F5a.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2 to 12
25
Fatigue Strength, MPa 130 to 210
380
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 280 to 330
450
Tensile Strength: Ultimate (UTS), MPa 490 to 570
710
Tensile Strength: Yield (Proof), MPa 390 to 500
520

Thermal Properties

Latent Heat of Fusion, J/g 370
260
Maximum Temperature: Mechanical, °C 190
510
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 490
1420
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
8.2
Electrical Conductivity: Equal Weight (Specific), % IACS 100
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
4.5
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
1.8
Embodied Energy, MJ/kg 150
24
Embodied Water, L/kg 1120
69

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
160
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
700
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
25
Strength to Weight: Bending, points 45 to 50
23
Thermal Diffusivity, mm2/s 54
11
Thermal Shock Resistance, points 21 to 25
20

Alloy Composition


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Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.25
Chromium (Cr), % 0 to 0.040
4.0 to 6.0
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
91.4 to 95.6
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 0.6
Molybdenum (Mo), % 0
0.44 to 0.65
Nickel (Ni), % 0
0 to 0.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0