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S13800 Stainless Steel vs. 2036 Aluminum

S13800 stainless steel belongs to the iron alloys classification, while 2036 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 S13800 stainless steel and the bottom bar is 2036 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 11 to 18
24
Fatigue Strength, MPa 410 to 870
130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 610 to 1030
210
Tensile Strength: Ultimate (UTS), MPa 980 to 1730
340
Tensile Strength: Yield (Proof), MPa 660 to 1580
200

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Mechanical, °C 810
190
Melting Completion (Liquidus), °C 1450
650
Melting Onset (Solidus), °C 1410
560
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 16
160
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
41
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
130

Otherwise Unclassified Properties

Base Metal Price, % relative 15
10
Density, g/cm3 7.9
2.9
Embodied Carbon, kg CO2/kg material 3.4
8.1
Embodied Energy, MJ/kg 46
150
Embodied Water, L/kg 140
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 190
70
Resilience: Unit (Modulus of Resilience), kJ/m3 1090 to 5490
270
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
48
Strength to Weight: Axial, points 35 to 61
33
Strength to Weight: Bending, points 28 to 41
38
Thermal Diffusivity, mm2/s 4.3
62
Thermal Shock Resistance, points 33 to 58
15

Alloy Composition


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Aluminum (Al), % 0.9 to 1.4
94.4 to 97.4
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 12.3 to 13.2
0 to 0.1
Copper (Cu), % 0
2.2 to 3.0
Iron (Fe), % 73.6 to 77.3
0 to 0.5
Magnesium (Mg), % 0
0.3 to 0.6
Manganese (Mn), % 0 to 0.2
0.1 to 0.4
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 7.5 to 8.5
0
Nitrogen (N), % 0 to 0.010
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0 to 0.0080
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15