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358.0 Aluminum vs. S44800 Stainless Steel

358.0 aluminum belongs to the aluminum alloys classification, while S44800 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 358.0 aluminum and the bottom bar is S44800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
210
Elongation at Break, % 3.5 to 6.0
23
Fatigue Strength, MPa 100 to 110
300
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 27
82
Shear Strength, MPa 300 to 320
370
Tensile Strength: Ultimate (UTS), MPa 350 to 370
590
Tensile Strength: Yield (Proof), MPa 290 to 320
450

Thermal Properties

Latent Heat of Fusion, J/g 520
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 560
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 150
17
Thermal Expansion, µm/m-K 21
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 130
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 19
19
Density, g/cm3 2.6
7.8
Embodied Carbon, kg CO2/kg material 8.7
3.8
Embodied Energy, MJ/kg 160
52
Embodied Water, L/kg 1090
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 20
120
Resilience: Unit (Modulus of Resilience), kJ/m3 590 to 710
480
Stiffness to Weight: Axial, points 15
15
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 37 to 39
21
Strength to Weight: Bending, points 42 to 44
20
Thermal Diffusivity, mm2/s 63
4.6
Thermal Shock Resistance, points 16 to 17
19

Alloy Composition

Aluminum (Al), % 89.1 to 91.8
0
Beryllium (Be), % 0.1 to 0.3
0
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0 to 0.2
28 to 30
Copper (Cu), % 0 to 0.2
0 to 0.15
Iron (Fe), % 0 to 0.3
62.6 to 66.5
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.2
0 to 0.3
Molybdenum (Mo), % 0
3.5 to 4.2
Nickel (Ni), % 0
2.0 to 2.5
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 7.6 to 8.6
0 to 0.2
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0.1 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0