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2218 Aluminum vs. ASTM A387 Grade 22 Steel

2218 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 22 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 2218 aluminum and the bottom bar is ASTM A387 grade 22 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 95 to 110
150 to 180
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 6.8 to 10
21
Fatigue Strength, MPa 110
160 to 240
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Shear Strength, MPa 210 to 250
300 to 380
Tensile Strength: Ultimate (UTS), MPa 330 to 430
480 to 600
Tensile Strength: Yield (Proof), MPa 260 to 310
230 to 350

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 220
460
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 510
1430
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 140
40
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 110
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 11
3.8
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.2
1.7
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1130
58

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 31
85 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 650
140 to 320
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 30 to 39
17 to 21
Strength to Weight: Bending, points 34 to 41
17 to 20
Thermal Diffusivity, mm2/s 52
11
Thermal Shock Resistance, points 15 to 19
14 to 17

Alloy Composition


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Aluminum (Al), % 88.8 to 93.6
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0 to 0.1
2.0 to 2.5
Copper (Cu), % 3.5 to 4.5
0
Iron (Fe), % 0 to 1.0
95.1 to 96.8
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.2
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 1.7 to 2.3
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.9
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0