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EN 1.4662 Stainless Steel vs. A206.0 Aluminum

EN 1.4662 stainless steel belongs to the iron alloys classification, while A206.0 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 EN 1.4662 stainless steel and the bottom bar is A206.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 28
4.2 to 10
Fatigue Strength, MPa 430 to 450
90 to 180
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 520 to 540
260
Tensile Strength: Ultimate (UTS), MPa 810 to 830
390 to 440
Tensile Strength: Yield (Proof), MPa 580 to 620
250 to 380

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 1090
170
Melting Completion (Liquidus), °C 1430
670
Melting Onset (Solidus), °C 1380
550
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 15
130
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
30
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
90

Otherwise Unclassified Properties

Base Metal Price, % relative 16
11
Density, g/cm3 7.7
3.0
Embodied Carbon, kg CO2/kg material 3.2
8.0
Embodied Energy, MJ/kg 45
150
Embodied Water, L/kg 170
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
16 to 37
Resilience: Unit (Modulus of Resilience), kJ/m3 840 to 940
440 to 1000
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 29 to 30
36 to 41
Strength to Weight: Bending, points 25
39 to 43
Thermal Diffusivity, mm2/s 3.9
48
Thermal Shock Resistance, points 22
17 to 19

Alloy Composition

Aluminum (Al), % 0
93.9 to 95.7
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 23 to 25
0
Copper (Cu), % 0.1 to 0.8
4.2 to 5.0
Iron (Fe), % 62.6 to 70.2
0 to 0.1
Magnesium (Mg), % 0
0 to 0.15
Manganese (Mn), % 2.5 to 4.0
0 to 0.2
Molybdenum (Mo), % 1.0 to 2.0
0
Nickel (Ni), % 3.0 to 4.5
0 to 0.050
Nitrogen (N), % 0.2 to 0.3
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.7
0 to 0.050
Sulfur (S), % 0 to 0.0050
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0
0.15 to 0.3
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15