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6005 Aluminum vs. EN 1.4558 Stainless Steel

6005 aluminum belongs to the aluminum alloys classification, while EN 1.4558 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 6005 aluminum and the bottom bar is EN 1.4558 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 9.5 to 17
39
Fatigue Strength, MPa 55 to 95
170
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 120 to 210
350
Tensile Strength: Ultimate (UTS), MPa 190 to 310
510
Tensile Strength: Yield (Proof), MPa 100 to 280
200

Thermal Properties

Latent Heat of Fusion, J/g 410
300
Maximum Temperature: Mechanical, °C 160
1100
Melting Completion (Liquidus), °C 650
1400
Melting Onset (Solidus), °C 610
1350
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 180 to 200
12
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 180
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.3
5.5
Embodied Energy, MJ/kg 150
77
Embodied Water, L/kg 1180
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 36
160
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 550
100
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 20 to 32
18
Strength to Weight: Bending, points 28 to 38
18
Thermal Diffusivity, mm2/s 74 to 83
3.1
Thermal Shock Resistance, points 8.6 to 14
12

Alloy Composition

Aluminum (Al), % 97.5 to 99
0.15 to 0.45
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.1
20 to 23
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.35
39.2 to 47.9
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Nickel (Ni), % 0
32 to 35
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.6 to 0.9
0 to 0.7
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0 to 0.6
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0