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S20161 Stainless Steel vs. 2219 Aluminum

S20161 stainless steel belongs to the iron alloys classification, while 2219 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 S20161 stainless steel and the bottom bar is 2219 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 46
2.2 to 20
Fatigue Strength, MPa 360
90 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 690
110 to 280
Tensile Strength: Ultimate (UTS), MPa 980
180 to 480
Tensile Strength: Yield (Proof), MPa 390
88 to 390

Thermal Properties

Latent Heat of Fusion, J/g 330
390
Maximum Temperature: Mechanical, °C 870
230
Melting Completion (Liquidus), °C 1380
640
Melting Onset (Solidus), °C 1330
540
Specific Heat Capacity, J/kg-K 490
870
Thermal Conductivity, W/m-K 15
110 to 170
Thermal Expansion, µm/m-K 16
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
28 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
81 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 12
11
Density, g/cm3 7.5
3.1
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 360
9.6 to 60
Resilience: Unit (Modulus of Resilience), kJ/m3 390
54 to 1060
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 26
44
Strength to Weight: Axial, points 36
16 to 43
Strength to Weight: Bending, points 29
23 to 44
Thermal Diffusivity, mm2/s 4.0
42 to 63
Thermal Shock Resistance, points 22
8.2 to 22

Alloy Composition

Aluminum (Al), % 0
91.5 to 93.8
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 15 to 18
0
Copper (Cu), % 0
5.8 to 6.8
Iron (Fe), % 65.6 to 73.9
0 to 0.3
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 4.0 to 6.0
0.2 to 0.4
Nickel (Ni), % 4.0 to 6.0
0
Nitrogen (N), % 0.080 to 0.2
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 3.0 to 4.0
0 to 0.2
Sulfur (S), % 0 to 0.040
0
Titanium (Ti), % 0
0.020 to 0.1
Vanadium (V), % 0
0.050 to 0.15
Zinc (Zn), % 0
0 to 0.1
Zirconium (Zr), % 0
0.1 to 0.25
Residuals, % 0
0 to 0.15