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6463 Aluminum vs. EN 1.4806 Stainless Steel

6463 aluminum belongs to the aluminum alloys classification, while EN 1.4806 stainless steel belongs to the iron 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 6463 aluminum and the bottom bar is EN 1.4806 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 42 to 74
140
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 9.0 to 17
6.8
Fatigue Strength, MPa 45 to 76
120
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
75
Tensile Strength: Ultimate (UTS), MPa 140 to 230
470
Tensile Strength: Yield (Proof), MPa 82 to 200
250

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 160
1000
Melting Completion (Liquidus), °C 660
1380
Melting Onset (Solidus), °C 620
1340
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 190 to 210
12
Thermal Expansion, µm/m-K 23
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 50 to 55
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 170 to 180
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.3
5.4
Embodied Energy, MJ/kg 150
76
Embodied Water, L/kg 1190
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17 to 25
27
Resilience: Unit (Modulus of Resilience), kJ/m3 50 to 300
160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 14 to 24
16
Strength to Weight: Bending, points 22 to 31
17
Thermal Diffusivity, mm2/s 79 to 86
3.1
Thermal Shock Resistance, points 6.3 to 10
11

Alloy Composition

Aluminum (Al), % 97.9 to 99.4
0
Carbon (C), % 0
0.3 to 0.5
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.15
40.4 to 48.7
Magnesium (Mg), % 0.45 to 0.9
0
Manganese (Mn), % 0 to 0.050
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
34 to 36
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.2 to 0.6
1.0 to 2.5
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.15
0