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S44536 Stainless Steel vs. 5049 Aluminum

S44536 stainless steel belongs to the iron alloys classification, while 5049 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 S44536 stainless steel and the bottom bar is 5049 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170
52 to 88
Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 22
2.0 to 18
Fatigue Strength, MPa 190
79 to 130
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 78
26
Shear Strength, MPa 290
130 to 190
Tensile Strength: Ultimate (UTS), MPa 460
210 to 330
Tensile Strength: Yield (Proof), MPa 280
91 to 280

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 990
190
Melting Completion (Liquidus), °C 1440
650
Melting Onset (Solidus), °C 1390
620
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 21
140
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.6
35
Electrical Conductivity: Equal Weight (Specific), % IACS 3.0
110

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 2.8
8.5
Embodied Energy, MJ/kg 41
150
Embodied Water, L/kg 140
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 89
6.0 to 31
Resilience: Unit (Modulus of Resilience), kJ/m3 200
59 to 570
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 17
22 to 34
Strength to Weight: Bending, points 17
29 to 39
Thermal Diffusivity, mm2/s 5.6
56
Thermal Shock Resistance, points 16
9.3 to 15

Alloy Composition

Aluminum (Al), % 0
94.7 to 97.9
Carbon (C), % 0 to 0.015
0
Chromium (Cr), % 20 to 23
0 to 0.3
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 72.8 to 80
0 to 0.5
Magnesium (Mg), % 0
1.6 to 2.5
Manganese (Mn), % 0 to 1.0
0.5 to 1.1
Nickel (Ni), % 0 to 0.5
0
Niobium (Nb), % 0.050 to 0.8
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0 to 0.8
0 to 0.1
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15