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S32654 Stainless Steel vs. 5457 Aluminum

S32654 stainless steel belongs to the iron alloys classification, while 5457 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 S32654 stainless steel and the bottom bar is 5457 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 220
32 to 55
Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 45
6.0 to 22
Fatigue Strength, MPa 450
55 to 98
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 82
26
Shear Strength, MPa 590
85 to 130
Tensile Strength: Ultimate (UTS), MPa 850
130 to 210
Tensile Strength: Yield (Proof), MPa 490
50 to 190

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 1100
180
Melting Completion (Liquidus), °C 1450
660
Melting Onset (Solidus), °C 1410
630
Specific Heat Capacity, J/kg-K 460
900
Thermal Conductivity, W/m-K 11
180
Thermal Expansion, µm/m-K 15
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
46
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
150

Otherwise Unclassified Properties

Base Metal Price, % relative 34
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 6.4
8.4
Embodied Energy, MJ/kg 87
160
Embodied Water, L/kg 220
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 330
12 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 570
18 to 250
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 29
13 to 21
Strength to Weight: Bending, points 25
21 to 28
Thermal Diffusivity, mm2/s 2.9
72
Thermal Shock Resistance, points 19
5.7 to 9.0

Alloy Composition


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Aluminum (Al), % 0
97.8 to 99.05
Carbon (C), % 0 to 0.020
0
Chromium (Cr), % 24 to 25
0
Copper (Cu), % 0.3 to 0.6
0 to 0.2
Iron (Fe), % 38.3 to 45.3
0 to 0.1
Magnesium (Mg), % 0
0.8 to 1.2
Manganese (Mn), % 2.0 to 4.0
0.15 to 0.45
Molybdenum (Mo), % 7.0 to 8.0
0
Nickel (Ni), % 21 to 23
0
Nitrogen (N), % 0.45 to 0.55
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.5
0 to 0.080
Sulfur (S), % 0 to 0.0050
0
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050
Residuals, % 0
0 to 0.1