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1080 Aluminum vs. ASTM A182 Grade F5

1080 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F5 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 1080 aluminum and the bottom bar is ASTM A182 grade F5.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 4.6 to 40
22
Fatigue Strength, MPa 21 to 48
220
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 49 to 78
340
Tensile Strength: Ultimate (UTS), MPa 72 to 130
540
Tensile Strength: Yield (Proof), MPa 17 to 120
310

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 170
510
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 640
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 230
40
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
8.1
Electrical Conductivity: Equal Weight (Specific), % IACS 200
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.8
Embodied Energy, MJ/kg 160
24
Embodied Water, L/kg 1200
69

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.7 to 21
100
Resilience: Unit (Modulus of Resilience), kJ/m3 2.1 to 100
260
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 7.4 to 14
19
Strength to Weight: Bending, points 14 to 22
19
Thermal Diffusivity, mm2/s 94
11
Thermal Shock Resistance, points 3.2 to 6.0
15

Alloy Composition


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Aluminum (Al), % 99.8 to 100
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
4.0 to 6.0
Copper (Cu), % 0 to 0.030
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.15
91.5 to 95.3
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0 to 0.020
0.3 to 0.6
Molybdenum (Mo), % 0
0.44 to 0.65
Nickel (Ni), % 0
0 to 0.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.15
0 to 0.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.030
0
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.030
0
Residuals, % 0 to 0.020
0