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EN 1.4618 Stainless Steel vs. 2117 Aluminum

EN 1.4618 stainless steel belongs to the iron alloys classification, while 2117 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 2117 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 210
70
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 51
26
Fatigue Strength, MPa 240 to 250
95
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 480 to 500
200
Tensile Strength: Ultimate (UTS), MPa 680 to 700
300
Tensile Strength: Yield (Proof), MPa 250 to 260
170

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 900
220
Melting Completion (Liquidus), °C 1400
650
Melting Onset (Solidus), °C 1360
550
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 15
150
Thermal Expansion, µm/m-K 16
24

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
8.2
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 150
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270 to 280
64
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 170
190
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 24 to 25
28
Strength to Weight: Bending, points 22 to 23
33
Thermal Diffusivity, mm2/s 4.0
59
Thermal Shock Resistance, points 15 to 16
12

Alloy Composition

Aluminum (Al), % 0
91 to 97.6
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
2.2 to 4.5
Iron (Fe), % 62.7 to 72.5
0 to 0.7
Magnesium (Mg), % 0
0.2 to 1.0
Manganese (Mn), % 5.5 to 9.5
0.4 to 1.0
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
0.2 to 0.8
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0
0 to 0.25
Residuals, % 0
0 to 0.15