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EN 1.4634 Stainless Steel vs. 6066 Aluminum

EN 1.4634 stainless steel belongs to the iron alloys classification, while 6066 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 1.4634 stainless steel and the bottom bar is 6066 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 21
7.8 to 17
Fatigue Strength, MPa 180
94 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 340
95 to 240
Tensile Strength: Ultimate (UTS), MPa 540
160 to 400
Tensile Strength: Yield (Proof), MPa 280
93 to 360

Thermal Properties

Latent Heat of Fusion, J/g 290
410
Maximum Temperature: Mechanical, °C 900
170
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1390
560
Specific Heat Capacity, J/kg-K 480
890
Thermal Conductivity, W/m-K 21
150
Thermal Expansion, µm/m-K 10
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
40
Electrical Conductivity: Equal Weight (Specific), % IACS 3.0
130

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.7
2.8
Embodied Carbon, kg CO2/kg material 2.9
8.3
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 140
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 93
23 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 200
61 to 920
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
49
Strength to Weight: Axial, points 20
16 to 39
Strength to Weight: Bending, points 19
23 to 43
Thermal Diffusivity, mm2/s 5.8
61
Thermal Shock Resistance, points 19
6.9 to 17

Alloy Composition


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Aluminum (Al), % 0.2 to 1.5
93 to 97
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 17.5 to 18.5
0 to 0.4
Copper (Cu), % 0 to 0.5
0.7 to 1.2
Iron (Fe), % 74.9 to 81.8
0 to 0.5
Magnesium (Mg), % 0
0.8 to 1.4
Manganese (Mn), % 0 to 1.0
0.6 to 1.1
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 0 to 0.5
0
Niobium (Nb), % 0.3 to 1.0
0
Phosphorus (P), % 0 to 0.050
0
Silicon (Si), % 0.2 to 1.5
0.9 to 1.8
Sulfur (S), % 0 to 0.050
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15