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1350 Aluminum vs. S44660 Stainless Steel

1350 aluminum belongs to the aluminum alloys classification, while S44660 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 1350 aluminum and the bottom bar is S44660 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 20 to 45
210
Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 1.4 to 30
20
Fatigue Strength, MPa 24 to 50
330
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 26
81
Shear Strength, MPa 44 to 110
410
Tensile Strength: Ultimate (UTS), MPa 68 to 190
660
Tensile Strength: Yield (Proof), MPa 25 to 170
510

Thermal Properties

Latent Heat of Fusion, J/g 400
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 650
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 230
17
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
21
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.3
4.3
Embodied Energy, MJ/kg 160
61
Embodied Water, L/kg 1200
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
120
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
640
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 7.0 to 19
24
Strength to Weight: Bending, points 14 to 27
22
Thermal Diffusivity, mm2/s 96
4.5
Thermal Shock Resistance, points 3.0 to 8.2
21

Alloy Composition


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Aluminum (Al), % 99.5 to 100
0
Boron (B), % 0 to 0.050
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.010
25 to 28
Copper (Cu), % 0 to 0.050
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
60.4 to 71
Manganese (Mn), % 0 to 0.010
0 to 1.0
Molybdenum (Mo), % 0
3.0 to 4.0
Nickel (Ni), % 0
1.0 to 3.5
Niobium (Nb), % 0
0.2 to 1.0
Nitrogen (N), % 0
0 to 0.040
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.020
0.2 to 1.0
Vanadium (V), % 0 to 0.020
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0