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S31266 Stainless Steel vs. 242.0 Aluminum

S31266 stainless steel belongs to the iron alloys classification, while 242.0 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 S31266 stainless steel and the bottom bar is 242.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
73
Elongation at Break, % 40
0.5 to 1.5
Fatigue Strength, MPa 400
55 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 81
27
Shear Strength, MPa 590
150 to 240
Tensile Strength: Ultimate (UTS), MPa 860
180 to 290
Tensile Strength: Yield (Proof), MPa 470
120 to 220

Thermal Properties

Latent Heat of Fusion, J/g 310
390
Maximum Temperature: Mechanical, °C 1100
210
Melting Completion (Liquidus), °C 1470
640
Melting Onset (Solidus), °C 1420
530
Specific Heat Capacity, J/kg-K 460
870
Thermal Conductivity, W/m-K 12
130 to 170
Thermal Expansion, µm/m-K 16
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.8
33 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
96 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 37
12
Density, g/cm3 8.2
3.1
Embodied Carbon, kg CO2/kg material 6.5
8.3
Embodied Energy, MJ/kg 89
150
Embodied Water, L/kg 220
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 290
1.3 to 3.4
Resilience: Unit (Modulus of Resilience), kJ/m3 540
110 to 340
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 29
16 to 26
Strength to Weight: Bending, points 24
23 to 32
Thermal Diffusivity, mm2/s 3.1
50 to 62
Thermal Shock Resistance, points 18
8.0 to 13

Alloy Composition

Aluminum (Al), % 0
88.4 to 93.6
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 23 to 25
0 to 0.25
Copper (Cu), % 1.0 to 2.5
3.5 to 4.5
Iron (Fe), % 34.1 to 46
0 to 1.0
Magnesium (Mg), % 0
1.2 to 1.8
Manganese (Mn), % 2.0 to 4.0
0 to 0.35
Molybdenum (Mo), % 5.2 to 6.2
0
Nickel (Ni), % 21 to 24
1.7 to 2.3
Nitrogen (N), % 0.35 to 0.6
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.0
0 to 0.7
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.25
Tungsten (W), % 1.5 to 2.5
0
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15