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2218 Aluminum vs. S44800 Stainless Steel

2218 aluminum belongs to the aluminum alloys classification, while S44800 stainless steel belongs to the iron alloys. There are 31 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 2218 aluminum and the bottom bar is S44800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 95 to 110
190
Elastic (Young's, Tensile) Modulus, GPa 73
210
Elongation at Break, % 6.8 to 10
23
Fatigue Strength, MPa 110
300
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 27
82
Shear Strength, MPa 210 to 250
370
Tensile Strength: Ultimate (UTS), MPa 330 to 430
590
Tensile Strength: Yield (Proof), MPa 260 to 310
450

Thermal Properties

Latent Heat of Fusion, J/g 390
300
Maximum Temperature: Mechanical, °C 220
1100
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 510
1410
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140
17
Thermal Expansion, µm/m-K 22
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 11
19
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
3.8
Embodied Energy, MJ/kg 150
52
Embodied Water, L/kg 1130
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 31
120
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 650
480
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 30 to 39
21
Strength to Weight: Bending, points 34 to 41
20
Thermal Diffusivity, mm2/s 52
4.6
Thermal Shock Resistance, points 15 to 19
19

Alloy Composition


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Aluminum (Al), % 88.8 to 93.6
0
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0 to 0.1
28 to 30
Copper (Cu), % 3.5 to 4.5
0 to 0.15
Iron (Fe), % 0 to 1.0
62.6 to 66.5
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.2
0 to 0.3
Molybdenum (Mo), % 0
3.5 to 4.2
Nickel (Ni), % 1.7 to 2.3
2.0 to 2.5
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.9
0 to 0.2
Sulfur (S), % 0
0 to 0.020
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0