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ASTM A182 Grade F122 vs. 1060 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 1060 aluminum belongs to the aluminum 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 ASTM A182 grade F122 and the bottom bar is 1060 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 23
1.1 to 30
Fatigue Strength, MPa 320
15 to 50
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
42 to 75
Tensile Strength: Ultimate (UTS), MPa 710
67 to 130
Tensile Strength: Yield (Proof), MPa 450
17 to 110

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 600
170
Melting Completion (Liquidus), °C 1490
660
Melting Onset (Solidus), °C 1440
650
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 24
230
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
62
Electrical Conductivity: Equal Weight (Specific), % IACS 12
210

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 3.0
8.3
Embodied Energy, MJ/kg 44
160
Embodied Water, L/kg 100
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
0.57 to 37
Resilience: Unit (Modulus of Resilience), kJ/m3 520
2.1 to 89
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25
6.9 to 13
Strength to Weight: Bending, points 22
14 to 21
Thermal Diffusivity, mm2/s 6.4
96
Thermal Shock Resistance, points 19
3.0 to 5.6

Alloy Composition

Aluminum (Al), % 0 to 0.020
99.6 to 100
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0
Copper (Cu), % 0.3 to 1.7
0 to 0.050
Iron (Fe), % 81.3 to 87.7
0 to 0.35
Magnesium (Mg), % 0
0 to 0.030
Manganese (Mn), % 0 to 0.7
0 to 0.030
Molybdenum (Mo), % 0.25 to 0.6
0
Nickel (Ni), % 0 to 0.5
0
Niobium (Nb), % 0.040 to 0.1
0
Nitrogen (N), % 0.040 to 0.1
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.25
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.030
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0 to 0.050
Zinc (Zn), % 0
0 to 0.050
Zirconium (Zr), % 0 to 0.010
0