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A206.0 Aluminum vs. S35140 Stainless Steel

A206.0 aluminum belongs to the aluminum alloys classification, while S35140 stainless steel belongs to the iron 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 A206.0 aluminum and the bottom bar is S35140 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 110
210
Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 4.2 to 10
34
Fatigue Strength, MPa 90 to 180
250
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 260
460
Tensile Strength: Ultimate (UTS), MPa 390 to 440
690
Tensile Strength: Yield (Proof), MPa 250 to 380
310

Thermal Properties

Latent Heat of Fusion, J/g 390
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 670
1420
Melting Onset (Solidus), °C 550
1370
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
14
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 90
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 11
31
Density, g/cm3 3.0
8.0
Embodied Carbon, kg CO2/kg material 8.0
5.5
Embodied Energy, MJ/kg 150
78
Embodied Water, L/kg 1150
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 37
190
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 1000
250
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
24
Strength to Weight: Axial, points 36 to 41
24
Strength to Weight: Bending, points 39 to 43
22
Thermal Diffusivity, mm2/s 48
3.7
Thermal Shock Resistance, points 17 to 19
16

Alloy Composition

Aluminum (Al), % 93.9 to 95.7
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
20 to 22
Copper (Cu), % 4.2 to 5.0
0
Iron (Fe), % 0 to 0.1
44.1 to 52.7
Magnesium (Mg), % 0 to 0.15
0
Manganese (Mn), % 0 to 0.2
1.0 to 3.0
Molybdenum (Mo), % 0
1.0 to 2.0
Nickel (Ni), % 0 to 0.050
25 to 27
Niobium (Nb), % 0
0.25 to 0.75
Nitrogen (N), % 0
0.080 to 0.2
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.050
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0.15 to 0.3
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0