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EN 1.4618 Stainless Steel vs. 2025 Aluminum

EN 1.4618 stainless steel belongs to the iron alloys classification, while 2025 aluminum belongs to the aluminum alloys. There are 31 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 EN 1.4618 stainless steel and the bottom bar is 2025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 210
110
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 51
15
Fatigue Strength, MPa 240 to 250
130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 480 to 500
240
Tensile Strength: Ultimate (UTS), MPa 680 to 700
400
Tensile Strength: Yield (Proof), MPa 250 to 260
260

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 900
190
Melting Completion (Liquidus), °C 1400
640
Melting Onset (Solidus), °C 1360
520
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 15
150
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
120

Otherwise Unclassified Properties

Base Metal Price, % relative 13
10
Density, g/cm3 7.7
3.0
Embodied Carbon, kg CO2/kg material 2.7
7.9
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 150
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270 to 280
55
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 170
450
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 24 to 25
37
Strength to Weight: Bending, points 22 to 23
40
Thermal Diffusivity, mm2/s 4.0
58
Thermal Shock Resistance, points 15 to 16
18

Alloy Composition

Aluminum (Al), % 0
90.9 to 95.2
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 16.5 to 18.5
0 to 0.1
Copper (Cu), % 1.0 to 2.5
3.9 to 5.0
Iron (Fe), % 62.7 to 72.5
0 to 1.0
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 5.5 to 9.5
0.4 to 1.2
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
0.5 to 1.2
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15