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358.0 Aluminum vs. S21900 Stainless Steel

358.0 aluminum belongs to the aluminum alloys classification, while S21900 stainless steel belongs to the iron alloys. There are 30 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 358.0 aluminum and the bottom bar is S21900 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
200
Elongation at Break, % 3.5 to 6.0
50
Fatigue Strength, MPa 100 to 110
380
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Shear Strength, MPa 300 to 320
510
Tensile Strength: Ultimate (UTS), MPa 350 to 370
710
Tensile Strength: Yield (Proof), MPa 290 to 320
390

Thermal Properties

Latent Heat of Fusion, J/g 520
290
Maximum Temperature: Mechanical, °C 170
980
Melting Completion (Liquidus), °C 600
1400
Melting Onset (Solidus), °C 560
1350
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 150
14
Thermal Expansion, µm/m-K 21
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 19
15
Density, g/cm3 2.6
7.7
Embodied Carbon, kg CO2/kg material 8.7
3.0
Embodied Energy, MJ/kg 160
43
Embodied Water, L/kg 1090
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 20
300
Resilience: Unit (Modulus of Resilience), kJ/m3 590 to 710
380
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 37 to 39
26
Strength to Weight: Bending, points 42 to 44
23
Thermal Diffusivity, mm2/s 63
3.8
Thermal Shock Resistance, points 16 to 17
15

Alloy Composition

Aluminum (Al), % 89.1 to 91.8
0
Beryllium (Be), % 0.1 to 0.3
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.2
19 to 21.5
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.3
59.4 to 67.4
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.2
8.0 to 10
Nickel (Ni), % 0
5.5 to 7.5
Nitrogen (N), % 0
0.15 to 0.4
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 7.6 to 8.6
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0.1 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0