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355.0 Aluminum vs. EN 1.4482 Stainless Steel

355.0 aluminum belongs to the aluminum alloys classification, while EN 1.4482 stainless steel belongs to the iron alloys. There are 30 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 355.0 aluminum and the bottom bar is EN 1.4482 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
200
Elongation at Break, % 1.5 to 2.6
34
Fatigue Strength, MPa 55 to 70
420 to 450
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Shear Strength, MPa 150 to 240
510 to 530
Tensile Strength: Ultimate (UTS), MPa 200 to 260
770 to 800
Tensile Strength: Yield (Proof), MPa 150 to 190
530 to 570

Thermal Properties

Latent Heat of Fusion, J/g 470
290
Maximum Temperature: Mechanical, °C 180
980
Melting Completion (Liquidus), °C 620
1420
Melting Onset (Solidus), °C 560
1370
Specific Heat Capacity, J/kg-K 890
480
Thermal Conductivity, W/m-K 150 to 170
15
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38 to 43
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 120 to 140
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.0
2.7
Embodied Energy, MJ/kg 150
38
Embodied Water, L/kg 1120
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.7 to 5.9
230 to 250
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 250
690 to 820
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 20 to 27
28 to 29
Strength to Weight: Bending, points 28 to 33
24 to 25
Thermal Diffusivity, mm2/s 60 to 69
4.0
Thermal Shock Resistance, points 9.1 to 12
21 to 22

Alloy Composition

Aluminum (Al), % 90.3 to 94.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.25
19.5 to 21.5
Copper (Cu), % 1.0 to 1.5
0 to 1.0
Iron (Fe), % 0 to 0.6
66.1 to 74.9
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.5
4.0 to 6.0
Molybdenum (Mo), % 0
0.1 to 0.6
Nickel (Ni), % 0
1.5 to 3.5
Nitrogen (N), % 0
0.050 to 0.2
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 4.5 to 5.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0