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ASTM A182 Grade F122 vs. 5005A Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 5005A aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 5005A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 220
29 to 64
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 23
1.1 to 21
Fatigue Strength, MPa 320
38 to 82
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
71 to 130
Tensile Strength: Ultimate (UTS), MPa 710
110 to 230
Tensile Strength: Yield (Proof), MPa 450
43 to 210

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 600
180
Melting Completion (Liquidus), °C 1490
660
Melting Onset (Solidus), °C 1440
630
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 24
200
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
52
Electrical Conductivity: Equal Weight (Specific), % IACS 12
170

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
150
Embodied Water, L/kg 100
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
2.0 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 520
14 to 310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25
12 to 24
Strength to Weight: Bending, points 22
19 to 31
Thermal Diffusivity, mm2/s 6.4
82
Thermal Shock Resistance, points 19
5.0 to 10

Alloy Composition


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Aluminum (Al), % 0 to 0.020
97.5 to 99.3
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0 to 0.1
Copper (Cu), % 0.3 to 1.7
0 to 0.050
Iron (Fe), % 81.3 to 87.7
0 to 0.45
Magnesium (Mg), % 0
0.7 to 1.1
Manganese (Mn), % 0 to 0.7
0 to 0.15
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 0.3
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15