S36200 Stainless Steel vs. 2014 Aluminum
S36200 stainless steel belongs to the iron alloys classification, while 2014 aluminum belongs to the aluminum alloys. There are 30 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 S36200 stainless steel and the bottom bar is 2014 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
72 |
Elongation at Break, % | 3.4 to 4.6 | |
1.5 to 16 |
Fatigue Strength, MPa | 450 to 570 | |
90 to 160 |
Poisson's Ratio | 0.28 | |
0.33 |
Shear Modulus, GPa | 76 | |
27 |
Shear Strength, MPa | 680 to 810 | |
130 to 290 |
Tensile Strength: Ultimate (UTS), MPa | 1180 to 1410 | |
190 to 500 |
Tensile Strength: Yield (Proof), MPa | 960 to 1240 | |
100 to 440 |
Thermal Properties
Latent Heat of Fusion, J/g | 280 | |
400 |
Maximum Temperature: Mechanical, °C | 820 | |
210 |
Melting Completion (Liquidus), °C | 1440 | |
630 |
Melting Onset (Solidus), °C | 1400 | |
510 |
Specific Heat Capacity, J/kg-K | 480 | |
870 |
Thermal Conductivity, W/m-K | 16 | |
150 |
Thermal Expansion, µm/m-K | 11 | |
23 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
40 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
120 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 12 | |
11 |
Density, g/cm3 | 7.8 | |
3.0 |
Embodied Carbon, kg CO2/kg material | 2.8 | |
8.1 |
Embodied Energy, MJ/kg | 40 | |
150 |
Embodied Water, L/kg | 120 | |
1130 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 46 to 51 | |
6.6 to 56 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 2380 to 3930 | |
76 to 1330 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
46 |
Strength to Weight: Axial, points | 42 to 50 | |
18 to 46 |
Strength to Weight: Bending, points | 32 to 36 | |
25 to 46 |
Thermal Diffusivity, mm2/s | 4.3 | |
58 |
Thermal Shock Resistance, points | 40 to 48 | |
8.4 to 22 |
Alloy Composition
Aluminum (Al), % | 0 to 0.1 | |
90.4 to 95 |
Carbon (C), % | 0 to 0.050 | |
0 |
Chromium (Cr), % | 14 to 14.5 | |
0 to 0.1 |
Copper (Cu), % | 0 | |
3.9 to 5.0 |
Iron (Fe), % | 75.4 to 79.5 | |
0 to 0.7 |
Magnesium (Mg), % | 0 | |
0.2 to 0.8 |
Manganese (Mn), % | 0 to 0.5 | |
0.4 to 1.2 |
Molybdenum (Mo), % | 0 to 0.3 | |
0 |
Nickel (Ni), % | 6.5 to 7.0 | |
0 |
Phosphorus (P), % | 0 to 0.030 | |
0 |
Silicon (Si), % | 0 to 0.3 | |
0.5 to 1.2 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Titanium (Ti), % | 0.6 to 0.9 | |
0 to 0.15 |
Zinc (Zn), % | 0 | |
0 to 0.25 |
Zirconium (Zr), % | 0 | |
0 to 0.2 |
Residuals, % | 0 | |
0 to 0.15 |