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5251 Aluminum vs. S42300 Stainless Steel

5251 aluminum belongs to the aluminum alloys classification, while S42300 stainless steel belongs to the iron alloys. There are 31 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 5251 aluminum and the bottom bar is S42300 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 44 to 79
330
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 2.0 to 19
9.1
Fatigue Strength, MPa 59 to 110
440
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 110 to 160
650
Tensile Strength: Ultimate (UTS), MPa 180 to 280
1100
Tensile Strength: Yield (Proof), MPa 67 to 250
850

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 180
750
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 610
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 150
25
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
4.5
Electrical Conductivity: Equal Weight (Specific), % IACS 120
5.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.5
3.2
Embodied Energy, MJ/kg 150
44
Embodied Water, L/kg 1180
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.4 to 27
93
Resilience: Unit (Modulus of Resilience), kJ/m3 33 to 450
1840
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 18 to 29
39
Strength to Weight: Bending, points 26 to 35
30
Thermal Diffusivity, mm2/s 61
6.8
Thermal Shock Resistance, points 7.9 to 13
40

Alloy Composition


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Aluminum (Al), % 95.5 to 98.2
0
Carbon (C), % 0
0.27 to 0.32
Chromium (Cr), % 0 to 0.15
11 to 12
Copper (Cu), % 0 to 0.15
0
Iron (Fe), % 0 to 0.5
82 to 85.1
Magnesium (Mg), % 1.7 to 2.4
0
Manganese (Mn), % 0.1 to 0.5
1.0 to 1.4
Molybdenum (Mo), % 0
2.5 to 3.0
Nickel (Ni), % 0
0 to 0.5
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.4
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.15
0
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.15
0