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6008 Aluminum vs. EN 1.4107 Stainless Steel

6008 aluminum belongs to the aluminum alloys classification, while EN 1.4107 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 6008 aluminum and the bottom bar is EN 1.4107 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 9.1 to 17
18 to 21
Fatigue Strength, MPa 55 to 88
260 to 350
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 200 to 290
620 to 700
Tensile Strength: Yield (Proof), MPa 100 to 220
400 to 570

Thermal Properties

Latent Heat of Fusion, J/g 410
270
Maximum Temperature: Mechanical, °C 180
740
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 620
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 190
27
Thermal Expansion, µm/m-K 23
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 160
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.5
2.1
Embodied Energy, MJ/kg 160
30
Embodied Water, L/kg 1180
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 28
110 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 76 to 360
420 to 840
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 21 to 29
22 to 25
Strength to Weight: Bending, points 28 to 35
21 to 22
Thermal Diffusivity, mm2/s 77
7.2
Thermal Shock Resistance, points 9.0 to 13
22 to 25

Alloy Composition

Aluminum (Al), % 96.5 to 99.1
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.3
11.5 to 12.5
Copper (Cu), % 0 to 0.3
0 to 0.3
Iron (Fe), % 0 to 0.35
83.8 to 87.2
Magnesium (Mg), % 0.4 to 0.7
0
Manganese (Mn), % 0 to 0.3
0.5 to 0.8
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
0.8 to 1.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0.5 to 0.9
0 to 0.4
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0.050 to 0.2
0 to 0.080
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants