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EN 1.4826 Stainless Steel vs. 6005A Aluminum

EN 1.4826 stainless steel belongs to the iron alloys classification, while 6005A aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 1.4826 stainless steel and the bottom bar is 6005A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 9.1
8.6 to 17
Fatigue Strength, MPa 140
55 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Tensile Strength: Ultimate (UTS), MPa 500
190 to 300
Tensile Strength: Yield (Proof), MPa 260
100 to 270

Thermal Properties

Latent Heat of Fusion, J/g 310
410
Maximum Temperature: Mechanical, °C 950
170
Melting Completion (Liquidus), °C 1400
650
Melting Onset (Solidus), °C 1360
600
Specific Heat Capacity, J/kg-K 490
900
Thermal Conductivity, W/m-K 14
180 to 190
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.0
47 to 50
Electrical Conductivity: Equal Weight (Specific), % IACS 2.4
150 to 170

Otherwise Unclassified Properties

Base Metal Price, % relative 17
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 3.3
8.3
Embodied Energy, MJ/kg 47
150
Embodied Water, L/kg 160
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 39
24 to 29
Resilience: Unit (Modulus of Resilience), kJ/m3 170
76 to 530
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 18
20 to 30
Strength to Weight: Bending, points 18
27 to 36
Thermal Diffusivity, mm2/s 3.7
72 to 79
Thermal Shock Resistance, points 11
8.6 to 13

Alloy Composition

Aluminum (Al), % 0
96.5 to 99.1
Carbon (C), % 0.3 to 0.5
0
Chromium (Cr), % 21 to 23
0 to 0.3
Copper (Cu), % 0
0 to 0.3
Iron (Fe), % 60.4 to 68.7
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.7
Manganese (Mn), % 0 to 2.0
0 to 0.5
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 9.0 to 11
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 1.0 to 2.5
0.5 to 0.9
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15