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N08020 Stainless Steel vs. 6008 Aluminum

N08020 stainless steel belongs to the iron alloys classification, while 6008 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 N08020 stainless steel and the bottom bar is 6008 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 15 to 34
9.1 to 17
Fatigue Strength, MPa 210 to 240
55 to 88
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 380 to 410
120 to 170
Tensile Strength: Ultimate (UTS), MPa 610 to 620
200 to 290
Tensile Strength: Yield (Proof), MPa 270 to 420
100 to 220

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Maximum Temperature: Mechanical, °C 1100
180
Melting Completion (Liquidus), °C 1410
640
Melting Onset (Solidus), °C 1360
620
Specific Heat Capacity, J/kg-K 460
900
Thermal Conductivity, W/m-K 12
190
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.6
49
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
160

Otherwise Unclassified Properties

Base Metal Price, % relative 38
9.5
Density, g/cm3 8.2
2.7
Embodied Carbon, kg CO2/kg material 6.6
8.5
Embodied Energy, MJ/kg 92
160
Embodied Water, L/kg 220
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83 to 170
24 to 28
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 440
76 to 360
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 21
21 to 29
Strength to Weight: Bending, points 20
28 to 35
Thermal Diffusivity, mm2/s 3.2
77
Thermal Shock Resistance, points 15
9.0 to 13

Alloy Composition

Aluminum (Al), % 0
96.5 to 99.1
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 19 to 21
0 to 0.3
Copper (Cu), % 3.0 to 4.0
0 to 0.3
Iron (Fe), % 29.9 to 44
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.7
Manganese (Mn), % 0 to 2.0
0 to 0.3
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 32 to 38
0
Niobium (Nb), % 0 to 1.0
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0.5 to 0.9
Sulfur (S), % 0 to 0.035
0
Titanium (Ti), % 0
0 to 0.1
Vanadium (V), % 0
0.050 to 0.2
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15