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EN 1.4112 Stainless Steel vs. 206.0 Aluminum

EN 1.4112 stainless steel belongs to the iron alloys classification, while 206.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 1.4112 stainless steel and the bottom bar is 206.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 230
95 to 110
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 20
8.4 to 12
Fatigue Strength, MPa 280
88 to 210
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 470
260
Tensile Strength: Ultimate (UTS), MPa 750
330 to 440
Tensile Strength: Yield (Proof), MPa 430
190 to 350

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Mechanical, °C 910
170
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1390
570
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 15
120
Thermal Expansion, µm/m-K 10
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
33
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
99

Otherwise Unclassified Properties

Base Metal Price, % relative 10
11
Density, g/cm3 7.7
3.0
Embodied Carbon, kg CO2/kg material 2.6
8.0
Embodied Energy, MJ/kg 37
150
Embodied Water, L/kg 130
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130
24 to 49
Resilience: Unit (Modulus of Resilience), kJ/m3 480
270 to 840
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 27
30 to 40
Strength to Weight: Bending, points 24
35 to 42
Thermal Diffusivity, mm2/s 4.1
46
Thermal Shock Resistance, points 26
17 to 23

Alloy Composition


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Aluminum (Al), % 0
93.3 to 95.3
Carbon (C), % 0.85 to 1.0
0
Chromium (Cr), % 17 to 19
0
Copper (Cu), % 0
4.2 to 5.0
Iron (Fe), % 76.6 to 81.2
0 to 0.15
Magnesium (Mg), % 0
0.15 to 0.35
Manganese (Mn), % 0 to 1.0
0.2 to 0.5
Molybdenum (Mo), % 0.9 to 1.3
0
Nickel (Ni), % 0
0 to 0.050
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.1
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0
0.15 to 0.3
Vanadium (V), % 0.070 to 0.12
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15