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EN 1.4606 Stainless Steel vs. 354.0 Aluminum

EN 1.4606 stainless steel belongs to the iron alloys classification, while 354.0 aluminum belongs to the aluminum alloys. There are 29 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 1.4606 stainless steel and the bottom bar is 354.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 23 to 39
2.4 to 3.0
Fatigue Strength, MPa 240 to 420
92 to 120
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
27
Tensile Strength: Ultimate (UTS), MPa 600 to 1020
360 to 380
Tensile Strength: Yield (Proof), MPa 280 to 630
280 to 310

Thermal Properties

Latent Heat of Fusion, J/g 300
530
Maximum Temperature: Mechanical, °C 910
170
Melting Completion (Liquidus), °C 1430
600
Melting Onset (Solidus), °C 1380
550
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 14
130
Thermal Expansion, µm/m-K 11
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
32
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
110

Otherwise Unclassified Properties

Base Metal Price, % relative 26
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 6.0
7.8
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 170
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190 to 200
8.6 to 9.8
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 1010
540 to 670
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 24
52
Strength to Weight: Axial, points 21 to 36
37 to 39
Strength to Weight: Bending, points 20 to 28
42 to 44
Thermal Diffusivity, mm2/s 3.7
52
Thermal Shock Resistance, points 21 to 35
17 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.35
87.3 to 89.4
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13 to 16
0
Copper (Cu), % 0
1.6 to 2.0
Iron (Fe), % 49.2 to 59
0 to 0.2
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 1.0 to 2.0
0 to 0.1
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 1.0
8.6 to 9.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.9 to 2.3
0 to 0.2
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15