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7075 Aluminum vs. ASTM A182 Grade F5a

7075 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 (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 7075 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, % 1.8 to 12
25
Fatigue Strength, MPa 110 to 190
380
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 150 to 340
450
Tensile Strength: Ultimate (UTS), MPa 240 to 590
710
Tensile Strength: Yield (Proof), MPa 120 to 510
520

Thermal Properties

Latent Heat of Fusion, J/g 380
260
Maximum Temperature: Mechanical, °C 200
510
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 480
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 130
40
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
8.2
Electrical Conductivity: Equal Weight (Specific), % IACS 98
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
4.5
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.8
Embodied Energy, MJ/kg 150
24
Embodied Water, L/kg 1120
69

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.8 to 44
160
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 1870
700
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 22 to 54
25
Strength to Weight: Bending, points 28 to 52
23
Thermal Diffusivity, mm2/s 50
11
Thermal Shock Resistance, points 10 to 25
20

Alloy Composition

Aluminum (Al), % 86.9 to 91.4
0
Carbon (C), % 0
0 to 0.25
Chromium (Cr), % 0.18 to 0.28
4.0 to 6.0
Copper (Cu), % 1.2 to 2.0
0
Iron (Fe), % 0 to 0.5
91.4 to 95.6
Magnesium (Mg), % 2.1 to 2.9
0
Manganese (Mn), % 0 to 0.3
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 0.4
0 to 0.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 5.1 to 6.1
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0