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S32050 Stainless Steel vs. 5005 Aluminum

S32050 stainless steel belongs to the iron alloys classification, while 5005 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 S32050 stainless steel and the bottom bar is 5005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 220
28 to 64
Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 46
1.1 to 23
Fatigue Strength, MPa 340
38 to 86
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 81
26
Shear Strength, MPa 540
70 to 130
Tensile Strength: Ultimate (UTS), MPa 770
110 to 230
Tensile Strength: Yield (Proof), MPa 370
41 to 210

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 1100
180
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1410
630
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 12
200
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
52
Electrical Conductivity: Equal Weight (Specific), % IACS 2.1
170

Otherwise Unclassified Properties

Base Metal Price, % relative 31
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 6.0
8.3
Embodied Energy, MJ/kg 81
150
Embodied Water, L/kg 210
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 290
2.3 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 330
12 to 320
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 27
11 to 23
Strength to Weight: Bending, points 23
19 to 31
Thermal Diffusivity, mm2/s 3.3
82
Thermal Shock Resistance, points 17
4.9 to 10

Alloy Composition


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Aluminum (Al), % 0
97 to 99.5
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 22 to 24
0 to 0.1
Copper (Cu), % 0 to 0.4
0 to 0.2
Iron (Fe), % 43.1 to 51.8
0 to 0.7
Magnesium (Mg), % 0
0.5 to 1.1
Manganese (Mn), % 0 to 1.5
0 to 0.2
Molybdenum (Mo), % 6.0 to 6.6
0
Nickel (Ni), % 20 to 23
0
Nitrogen (N), % 0.21 to 0.32
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.0
0 to 0.3
Sulfur (S), % 0 to 0.020
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15