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EN AC-45500 Aluminum vs. EN 1.4006 Stainless Steel

EN AC-45500 aluminum belongs to the aluminum alloys classification, while EN 1.4006 stainless steel belongs to the iron alloys. There are 29 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 AC-45500 aluminum and the bottom bar is EN 1.4006 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.8
16 to 23
Fatigue Strength, MPa 80
150 to 300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 320
590 to 750
Tensile Strength: Yield (Proof), MPa 250
230 to 510

Thermal Properties

Latent Heat of Fusion, J/g 500
270
Maximum Temperature: Mechanical, °C 170
740
Melting Completion (Liquidus), °C 610
1440
Melting Onset (Solidus), °C 600
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 150
30
Thermal Expansion, µm/m-K 22
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 2.6
7.7
Embodied Carbon, kg CO2/kg material 8.0
1.9
Embodied Energy, MJ/kg 150
27
Embodied Water, L/kg 1110
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.2
99 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 430
140 to 660
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 34
21 to 27
Strength to Weight: Bending, points 40
20 to 24
Thermal Diffusivity, mm2/s 65
8.1
Thermal Shock Resistance, points 15
21 to 26

Alloy Composition


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Aluminum (Al), % 90.6 to 93.1
0
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0
11.5 to 13.5
Copper (Cu), % 0.2 to 0.7
0
Iron (Fe), % 0 to 0.25
83.1 to 88.4
Magnesium (Mg), % 0.2 to 0.45
0
Manganese (Mn), % 0 to 0.15
0 to 1.5
Nickel (Ni), % 0
0 to 0.75
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 6.5 to 7.5
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.070
0
Residuals, % 0 to 0.1
0