MakeItFrom.com
Menu (ESC)

N08800 Stainless Steel vs. 6008 Aluminum

N08800 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 (3, 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 N08800 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, % 4.5 to 34
9.1 to 17
Fatigue Strength, MPa 150 to 390
55 to 88
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 340 to 580
120 to 170
Tensile Strength: Ultimate (UTS), MPa 500 to 1000
200 to 290
Tensile Strength: Yield (Proof), MPa 190 to 830
100 to 220

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Maximum Temperature: Mechanical, °C 1100
180
Melting Completion (Liquidus), °C 1390
640
Melting Onset (Solidus), °C 1360
620
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 12
190
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
49
Electrical Conductivity: Equal Weight (Specific), % IACS 1.9
160

Otherwise Unclassified Properties

Base Metal Price, % relative 30
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 5.3
8.5
Embodied Energy, MJ/kg 76
160
Embodied Water, L/kg 200
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 160
24 to 28
Resilience: Unit (Modulus of Resilience), kJ/m3 96 to 1740
76 to 360
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 18 to 35
21 to 29
Strength to Weight: Bending, points 18 to 28
28 to 35
Thermal Diffusivity, mm2/s 3.0
77
Thermal Shock Resistance, points 13 to 25
9.0 to 13

Alloy Composition

Aluminum (Al), % 0.15 to 0.6
96.5 to 99.1
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 19 to 23
0 to 0.3
Copper (Cu), % 0 to 0.75
0 to 0.3
Iron (Fe), % 39.5 to 50.7
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.7
Manganese (Mn), % 0 to 1.5
0 to 0.3
Nickel (Ni), % 30 to 35
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0.5 to 0.9
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.15 to 0.6
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