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2618 Aluminum vs. AISI 420 Stainless Steel

2618 aluminum belongs to the aluminum alloys classification, while AISI 420 stainless steel belongs to the iron alloys. There are 31 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 2618 aluminum and the bottom bar is AISI 420 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
190
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 5.8
8.0 to 15
Fatigue Strength, MPa 110
220 to 670
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 260
420 to 1010
Tensile Strength: Ultimate (UTS), MPa 420
690 to 1720
Tensile Strength: Yield (Proof), MPa 350
380 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Mechanical, °C 210
620
Melting Completion (Liquidus), °C 640
1510
Melting Onset (Solidus), °C 550
1450
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 160
27
Thermal Expansion, µm/m-K 22
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
3.0
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.5

Otherwise Unclassified Properties

Base Metal Price, % relative 11
7.5
Density, g/cm3 2.9
7.7
Embodied Carbon, kg CO2/kg material 8.3
2.0
Embodied Energy, MJ/kg 150
28
Embodied Water, L/kg 1150
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23
88 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 850
380 to 4410
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 40
25 to 62
Strength to Weight: Bending, points 42
22 to 41
Thermal Diffusivity, mm2/s 62
7.3
Thermal Shock Resistance, points 19
25 to 62

Alloy Composition

Aluminum (Al), % 92.4 to 94.9
0
Carbon (C), % 0
0.15 to 0.4
Chromium (Cr), % 0
12 to 14
Copper (Cu), % 1.9 to 2.7
0
Iron (Fe), % 0.9 to 1.3
82.3 to 87.9
Magnesium (Mg), % 1.3 to 1.8
0
Manganese (Mn), % 0
0 to 1.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0.9 to 1.2
0 to 0.75
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.1 to 0.25
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0.040 to 0.1
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0