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ASTM A182 Grade F122 vs. 7003 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 7003 aluminum belongs to the aluminum 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 ASTM A182 grade F122 and the bottom bar is 7003 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 23
11
Fatigue Strength, MPa 320
130 to 150
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
210 to 230
Tensile Strength: Ultimate (UTS), MPa 710
350 to 390
Tensile Strength: Yield (Proof), MPa 450
300 to 310

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Maximum Temperature: Mechanical, °C 600
200
Melting Completion (Liquidus), °C 1490
630
Melting Onset (Solidus), °C 1440
510
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 24
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
36
Electrical Conductivity: Equal Weight (Specific), % IACS 12
110

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 8.0
2.9
Embodied Carbon, kg CO2/kg material 3.0
8.1
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
37 to 41
Resilience: Unit (Modulus of Resilience), kJ/m3 520
630 to 710
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
47
Strength to Weight: Axial, points 25
33 to 37
Strength to Weight: Bending, points 22
37 to 40
Thermal Diffusivity, mm2/s 6.4
59
Thermal Shock Resistance, points 19
15 to 17

Alloy Composition

Aluminum (Al), % 0 to 0.020
90.6 to 94.5
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0 to 0.2
Copper (Cu), % 0.3 to 1.7
0 to 0.2
Iron (Fe), % 81.3 to 87.7
0 to 0.35
Magnesium (Mg), % 0
0.5 to 1.0
Manganese (Mn), % 0 to 0.7
0 to 0.3
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 to 0.2
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0
Zinc (Zn), % 0
5.0 to 6.5
Zirconium (Zr), % 0 to 0.010
0.050 to 0.25
Residuals, % 0
0 to 0.15