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EN 1.4606 Stainless Steel vs. 6360 Aluminum

EN 1.4606 stainless steel belongs to the iron alloys classification, while 6360 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 1.4606 stainless steel and the bottom bar is 6360 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 23 to 39
9.0 to 18
Fatigue Strength, MPa 240 to 420
31 to 67
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 410 to 640
76 to 130
Tensile Strength: Ultimate (UTS), MPa 600 to 1020
120 to 220
Tensile Strength: Yield (Proof), MPa 280 to 630
57 to 170

Thermal Properties

Latent Heat of Fusion, J/g 300
400
Maximum Temperature: Mechanical, °C 910
160
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
630
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 14
210
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
54
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
180

Otherwise Unclassified Properties

Base Metal Price, % relative 26
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 6.0
8.3
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 170
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190 to 200
14 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 1010
24 to 210
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 21 to 36
13 to 23
Strength to Weight: Bending, points 20 to 28
20 to 30
Thermal Diffusivity, mm2/s 3.7
86
Thermal Shock Resistance, points 21 to 35
5.5 to 9.9

Alloy Composition

Aluminum (Al), % 0 to 0.35
97.8 to 99.3
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13 to 16
0 to 0.050
Copper (Cu), % 0
0 to 0.15
Iron (Fe), % 49.2 to 59
0.1 to 0.3
Magnesium (Mg), % 0
0.25 to 0.45
Manganese (Mn), % 1.0 to 2.0
0.020 to 0.15
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 1.0
0.35 to 0.8
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.9 to 2.3
0 to 0.1
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15