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EN 1.4062 Stainless Steel vs. 6081 Aluminum

EN 1.4062 stainless steel belongs to the iron alloys classification, while 6081 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 EN 1.4062 stainless steel and the bottom bar is 6081 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 23 to 34
9.0
Fatigue Strength, MPa 410 to 420
110
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 510
180
Tensile Strength: Ultimate (UTS), MPa 770 to 800
310
Tensile Strength: Yield (Proof), MPa 530 to 600
270

Thermal Properties

Latent Heat of Fusion, J/g 290
410
Maximum Temperature: Mechanical, °C 1030
160
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
610
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 15
180
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.1
47
Electrical Conductivity: Equal Weight (Specific), % IACS 2.4
160

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 2.6
8.3
Embodied Energy, MJ/kg 37
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 170 to 230
27
Resilience: Unit (Modulus of Resilience), kJ/m3 690 to 910
540
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 28 to 29
32
Strength to Weight: Bending, points 24 to 25
37
Thermal Diffusivity, mm2/s 4.0
74
Thermal Shock Resistance, points 21 to 22
14

Alloy Composition

Aluminum (Al), % 0
96.3 to 98.6
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 21.5 to 24
0 to 0.1
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 69.3 to 77.3
0 to 0.5
Magnesium (Mg), % 0
0.6 to 1.0
Manganese (Mn), % 0 to 2.0
0.1 to 0.45
Molybdenum (Mo), % 0 to 0.45
0
Nickel (Ni), % 1.0 to 2.9
0
Nitrogen (N), % 0.16 to 0.28
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0.7 to 1.1
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15