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EN 1.4618 Stainless Steel vs. 6025 Aluminum

EN 1.4618 stainless steel belongs to the iron alloys classification, while 6025 aluminum belongs to the aluminum alloys. There are 30 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 1.4618 stainless steel and the bottom bar is 6025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 51
2.8 to 10
Fatigue Strength, MPa 240 to 250
67 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 480 to 500
110 to 140
Tensile Strength: Ultimate (UTS), MPa 680 to 700
190 to 240
Tensile Strength: Yield (Proof), MPa 250 to 260
68 to 210

Thermal Properties

Latent Heat of Fusion, J/g 280
410
Maximum Temperature: Mechanical, °C 900
160
Melting Completion (Liquidus), °C 1400
650
Melting Onset (Solidus), °C 1360
550
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 15
130
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
33
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
110

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.7
2.8
Embodied Carbon, kg CO2/kg material 2.7
8.5
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 150
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270 to 280
6.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 170
33 to 310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 24 to 25
19 to 24
Strength to Weight: Bending, points 22 to 23
26 to 31
Thermal Diffusivity, mm2/s 4.0
54
Thermal Shock Resistance, points 15 to 16
8.2 to 10

Alloy Composition

Aluminum (Al), % 0
91.7 to 96.3
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 16.5 to 18.5
0 to 0.2
Copper (Cu), % 1.0 to 2.5
0.2 to 0.7
Iron (Fe), % 62.7 to 72.5
0 to 0.7
Magnesium (Mg), % 0
2.1 to 3.0
Manganese (Mn), % 5.5 to 9.5
0.6 to 1.4
Nickel (Ni), % 4.5 to 5.5
0
Nitrogen (N), % 0 to 0.15
0
Phosphorus (P), % 0 to 0.070
0
Silicon (Si), % 0 to 1.0
0.8 to 1.5
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.15