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5251 Aluminum vs. S32050 Stainless Steel

5251 aluminum belongs to the aluminum alloys classification, while S32050 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 S32050 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 44 to 79
220
Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 2.0 to 19
46
Fatigue Strength, MPa 59 to 110
340
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 110 to 160
540
Tensile Strength: Ultimate (UTS), MPa 180 to 280
770
Tensile Strength: Yield (Proof), MPa 67 to 250
370

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 610
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 150
12
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.5
6.0
Embodied Energy, MJ/kg 150
81
Embodied Water, L/kg 1180
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.4 to 27
290
Resilience: Unit (Modulus of Resilience), kJ/m3 33 to 450
330
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 18 to 29
27
Strength to Weight: Bending, points 26 to 35
23
Thermal Diffusivity, mm2/s 61
3.3
Thermal Shock Resistance, points 7.9 to 13
17

Alloy Composition

Aluminum (Al), % 95.5 to 98.2
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.15
22 to 24
Copper (Cu), % 0 to 0.15
0 to 0.4
Iron (Fe), % 0 to 0.5
43.1 to 51.8
Magnesium (Mg), % 1.7 to 2.4
0
Manganese (Mn), % 0.1 to 0.5
0 to 1.5
Molybdenum (Mo), % 0
6.0 to 6.6
Nickel (Ni), % 0
20 to 23
Nitrogen (N), % 0
0.21 to 0.32
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.15
0