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5657 Aluminum vs. S21900 Stainless Steel

5657 aluminum belongs to the aluminum alloys classification, while S21900 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 5657 aluminum and the bottom bar is S21900 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 50
220
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 6.6 to 15
50
Fatigue Strength, MPa 74 to 88
380
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 92 to 110
510
Tensile Strength: Ultimate (UTS), MPa 150 to 200
710
Tensile Strength: Yield (Proof), MPa 140 to 170
390

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 180
980
Melting Completion (Liquidus), °C 660
1400
Melting Onset (Solidus), °C 640
1350
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 210
14
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 180
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
15
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.4
3.0
Embodied Energy, MJ/kg 160
43
Embodied Water, L/kg 1200
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.7 to 27
300
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 200
380
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 15 to 20
26
Strength to Weight: Bending, points 23 to 28
23
Thermal Diffusivity, mm2/s 84
3.8
Thermal Shock Resistance, points 6.7 to 8.6
15

Alloy Composition

Aluminum (Al), % 98.5 to 99.4
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
19 to 21.5
Copper (Cu), % 0 to 0.1
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.1
59.4 to 67.4
Magnesium (Mg), % 0.6 to 1.0
0
Manganese (Mn), % 0 to 0.030
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), % 0 to 0.080
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.050
0