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EN 1.4310 Stainless Steel vs. 2018 Aluminum

EN 1.4310 stainless steel belongs to the iron alloys classification, while 2018 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 1.4310 stainless steel and the bottom bar is 2018 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 270
120
Elastic (Young's, Tensile) Modulus, GPa 200
73
Elongation at Break, % 14 to 45
9.6
Fatigue Strength, MPa 240 to 330
120
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 510 to 550
270
Tensile Strength: Ultimate (UTS), MPa 730 to 900
420
Tensile Strength: Yield (Proof), MPa 260 to 570
310

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 910
220
Melting Completion (Liquidus), °C 1420
640
Melting Onset (Solidus), °C 1380
510
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 15
150
Thermal Expansion, µm/m-K 18
22

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 14
11
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 2.9
8.1
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 140
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 260
37
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 830
670
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 26 to 32
38
Strength to Weight: Bending, points 23 to 27
41
Thermal Diffusivity, mm2/s 4.0
57
Thermal Shock Resistance, points 15 to 18
19

Alloy Composition

Aluminum (Al), % 0
89.7 to 94.4
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 16 to 19
0 to 0.1
Copper (Cu), % 0
3.5 to 4.5
Iron (Fe), % 66.4 to 78
0 to 1.0
Magnesium (Mg), % 0
0.45 to 0.9
Manganese (Mn), % 0 to 2.0
0 to 0.2
Molybdenum (Mo), % 0 to 0.8
0
Nickel (Ni), % 6.0 to 9.5
1.7 to 2.3
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 2.0
0 to 0.9
Sulfur (S), % 0 to 0.015
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15