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S32654 Stainless Steel vs. 5254 Aluminum

S32654 stainless steel belongs to the iron alloys classification, while 5254 aluminum belongs to the aluminum 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 S32654 stainless steel and the bottom bar is 5254 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 45
3.4 to 22
Fatigue Strength, MPa 450
110 to 160
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 82
26
Shear Strength, MPa 590
150 to 200
Tensile Strength: Ultimate (UTS), MPa 850
240 to 350
Tensile Strength: Yield (Proof), MPa 490
100 to 270

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 1100
190
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1410
590
Specific Heat Capacity, J/kg-K 460
900
Thermal Conductivity, W/m-K 11
130
Thermal Expansion, µm/m-K 15
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
32
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
110

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
8.8
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 220
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 330
11 to 41
Resilience: Unit (Modulus of Resilience), kJ/m3 570
73 to 550
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 29
25 to 37
Strength to Weight: Bending, points 25
32 to 41
Thermal Diffusivity, mm2/s 2.9
52
Thermal Shock Resistance, points 19
10 to 16

Alloy Composition


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Aluminum (Al), % 0
94.4 to 96.8
Carbon (C), % 0 to 0.020
0
Chromium (Cr), % 24 to 25
0.15 to 0.35
Copper (Cu), % 0.3 to 0.6
0 to 0.050
Iron (Fe), % 38.3 to 45.3
0 to 0.45
Magnesium (Mg), % 0
3.1 to 3.9
Manganese (Mn), % 2.0 to 4.0
0 to 0.010
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 0.45
Sulfur (S), % 0 to 0.0050
0
Titanium (Ti), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15