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EN 1.4962 Stainless Steel vs. 2618 Aluminum

EN 1.4962 stainless steel belongs to the iron alloys classification, while 2618 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 1.4962 stainless steel and the bottom bar is 2618 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 210
120
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 22 to 34
5.8
Fatigue Strength, MPa 210 to 330
110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 420 to 440
260
Tensile Strength: Ultimate (UTS), MPa 630 to 690
420
Tensile Strength: Yield (Proof), MPa 260 to 490
350

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Mechanical, °C 910
210
Melting Completion (Liquidus), °C 1480
640
Melting Onset (Solidus), °C 1440
550
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 14
160
Thermal Expansion, µm/m-K 16
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
37
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
110

Otherwise Unclassified Properties

Base Metal Price, % relative 23
11
Density, g/cm3 8.1
2.9
Embodied Carbon, kg CO2/kg material 4.1
8.3
Embodied Energy, MJ/kg 59
150
Embodied Water, L/kg 150
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 170
23
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 610
850
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
47
Strength to Weight: Axial, points 21 to 24
40
Strength to Weight: Bending, points 20 to 21
42
Thermal Diffusivity, mm2/s 3.7
62
Thermal Shock Resistance, points 14 to 16
19

Alloy Composition

Aluminum (Al), % 0
92.4 to 94.9
Boron (B), % 0.0015 to 0.0060
0
Carbon (C), % 0.070 to 0.15
0
Chromium (Cr), % 15.5 to 17.5
0
Copper (Cu), % 0
1.9 to 2.7
Iron (Fe), % 62.1 to 69
0.9 to 1.3
Magnesium (Mg), % 0
1.3 to 1.8
Manganese (Mn), % 0 to 1.5
0
Nickel (Ni), % 12.5 to 14.5
0.9 to 1.2
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.5
0.1 to 0.25
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.4 to 0.7
0.040 to 0.1
Tungsten (W), % 2.5 to 3.0
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15