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EN AC-43500 Aluminum vs. EN 1.4446 Stainless Steel

EN AC-43500 aluminum belongs to the aluminum alloys classification, while EN 1.4446 stainless steel belongs to the iron 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 AC-43500 aluminum and the bottom bar is EN 1.4446 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 68 to 91
140
Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 4.5 to 13
23
Fatigue Strength, MPa 62 to 100
160
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
79
Tensile Strength: Ultimate (UTS), MPa 220 to 300
490
Tensile Strength: Yield (Proof), MPa 140 to 170
240

Thermal Properties

Latent Heat of Fusion, J/g 550
290
Maximum Temperature: Mechanical, °C 170
980
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 590
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 140
14
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
22
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 7.8
4.5
Embodied Energy, MJ/kg 150
60
Embodied Water, L/kg 1070
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 26
93
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 200
140
Stiffness to Weight: Axial, points 16
14
Stiffness to Weight: Bending, points 54
25
Strength to Weight: Axial, points 24 to 33
17
Strength to Weight: Bending, points 32 to 39
17
Thermal Diffusivity, mm2/s 60
3.6
Thermal Shock Resistance, points 10 to 14
11

Alloy Composition

Aluminum (Al), % 86.4 to 90.5
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
16.5 to 18.5
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.25
59.7 to 66.9
Magnesium (Mg), % 0.1 to 0.6
0
Manganese (Mn), % 0.4 to 0.8
0 to 1.5
Molybdenum (Mo), % 0
4.0 to 4.5
Nickel (Ni), % 0
12.5 to 14.5
Nitrogen (N), % 0
0.12 to 0.22
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 9.0 to 11.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.070
0
Residuals, % 0 to 0.15
0