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AISI 302 Stainless Steel vs. 2618 Aluminum

AISI 302 stainless steel belongs to the iron alloys classification, while 2618 aluminum belongs to the aluminum 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 AISI 302 stainless steel and the bottom bar is 2618 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 440
120
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 4.5 to 46
5.8
Fatigue Strength, MPa 210 to 520
110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 400 to 830
260
Tensile Strength: Ultimate (UTS), MPa 580 to 1430
420
Tensile Strength: Yield (Proof), MPa 230 to 1100
350

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Mechanical, °C 710
210
Melting Completion (Liquidus), °C 1420
640
Melting Onset (Solidus), °C 1400
550
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 16
160
Thermal Expansion, µm/m-K 17
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
37
Electrical Conductivity: Equal Weight (Specific), % IACS 2.8
110

Otherwise Unclassified Properties

Base Metal Price, % relative 15
11
Density, g/cm3 7.8
2.9
Embodied Carbon, kg CO2/kg material 3.0
8.3
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 140
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 59 to 260
23
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 3070
850
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 21 to 51
40
Strength to Weight: Bending, points 20 to 36
42
Thermal Diffusivity, mm2/s 4.4
62
Thermal Shock Resistance, points 12 to 31
19

Alloy Composition


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Aluminum (Al), % 0
92.4 to 94.9
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 17 to 19
0
Copper (Cu), % 0
1.9 to 2.7
Iron (Fe), % 67.9 to 75
0.9 to 1.3
Magnesium (Mg), % 0
1.3 to 1.8
Manganese (Mn), % 0 to 2.0
0
Nickel (Ni), % 8.0 to 10
0.9 to 1.2
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0.1 to 0.25
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0.040 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15