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S44800 Stainless Steel vs. 5059 Aluminum

S44800 stainless steel belongs to the iron alloys classification, while 5059 aluminum belongs to the aluminum 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 S44800 stainless steel and the bottom bar is 5059 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
69
Elongation at Break, % 23
11 to 25
Fatigue Strength, MPa 300
170 to 240
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 82
26
Shear Strength, MPa 370
220 to 250
Tensile Strength: Ultimate (UTS), MPa 590
350 to 410
Tensile Strength: Yield (Proof), MPa 450
170 to 300

Thermal Properties

Latent Heat of Fusion, J/g 300
390
Maximum Temperature: Corrosion, °C 460
65
Maximum Temperature: Mechanical, °C 1100
210
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1410
510
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 17
110
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.6
29
Electrical Conductivity: Equal Weight (Specific), % IACS 3.0
95

Otherwise Unclassified Properties

Base Metal Price, % relative 19
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.8
9.1
Embodied Energy, MJ/kg 52
160
Embodied Water, L/kg 190
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
42 to 75
Resilience: Unit (Modulus of Resilience), kJ/m3 480
220 to 650
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 21
36 to 42
Strength to Weight: Bending, points 20
41 to 45
Thermal Diffusivity, mm2/s 4.6
44
Thermal Shock Resistance, points 19
16 to 18

Alloy Composition

Aluminum (Al), % 0
89.9 to 94
Carbon (C), % 0 to 0.010
0
Chromium (Cr), % 28 to 30
0 to 0.25
Copper (Cu), % 0 to 0.15
0 to 0.25
Iron (Fe), % 62.6 to 66.5
0 to 0.5
Magnesium (Mg), % 0
5.0 to 6.0
Manganese (Mn), % 0 to 0.3
0.6 to 1.2
Molybdenum (Mo), % 3.5 to 4.2
0
Nickel (Ni), % 2.0 to 2.5
0
Nitrogen (N), % 0 to 0.020
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.2
0 to 0.45
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0.4 to 0.9
Zirconium (Zr), % 0
0.050 to 0.25
Residuals, % 0
0 to 0.15