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6005 Aluminum vs. EN 1.4460 Stainless Steel

6005 aluminum belongs to the aluminum alloys classification, while EN 1.4460 stainless steel belongs to the iron alloys. There are 31 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 1.4460 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 90 to 95
220
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 9.5 to 17
21
Fatigue Strength, MPa 55 to 95
330
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 26
80
Shear Strength, MPa 120 to 210
470
Tensile Strength: Ultimate (UTS), MPa 190 to 310
750
Tensile Strength: Yield (Proof), MPa 100 to 280
510

Thermal Properties

Latent Heat of Fusion, J/g 410
300
Maximum Temperature: Mechanical, °C 160
1100
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 610
1390
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 180 to 200
15
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 180
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
18
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.3
3.4
Embodied Energy, MJ/kg 150
48
Embodied Water, L/kg 1180
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 36
140
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 550
640
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 20 to 32
27
Strength to Weight: Bending, points 28 to 38
24
Thermal Diffusivity, mm2/s 74 to 83
4.0
Thermal Shock Resistance, points 8.6 to 14
20

Alloy Composition

Aluminum (Al), % 97.5 to 99
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.1
25 to 28
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.35
60.2 to 69.2
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
0 to 2.0
Molybdenum (Mo), % 0
1.3 to 2.0
Nickel (Ni), % 0
4.5 to 6.5
Nitrogen (N), % 0
0.050 to 0.2
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0.6 to 0.9
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0