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EN 1.4301 Stainless Steel vs. 201.0 Aluminum

EN 1.4301 stainless steel belongs to the iron alloys classification, while 201.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 1.4301 stainless steel and the bottom bar is 201.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 270
95 to 140
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 14 to 46
4.4 to 20
Fatigue Strength, MPa 200 to 330
120 to 150
Impact Strength: V-Notched Charpy, J 91 to 94
10 to 22
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 430 to 550
290
Tensile Strength: Ultimate (UTS), MPa 610 to 900
370 to 470
Tensile Strength: Yield (Proof), MPa 220 to 570
220 to 400

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 940
170
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1380
570
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 15
120
Thermal Expansion, µm/m-K 16
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
30 to 33
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
87 to 97

Otherwise Unclassified Properties

Base Metal Price, % relative 15
38
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 3.0
8.7
Embodied Energy, MJ/kg 43
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 220
19 to 63
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 820
330 to 1160
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 22 to 32
33 to 42
Strength to Weight: Bending, points 20 to 27
37 to 44
Thermal Diffusivity, mm2/s 4.0
45
Thermal Shock Resistance, points 14 to 20
19 to 25

Alloy Composition

Aluminum (Al), % 0
92.1 to 95.1
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 17.5 to 19.5
0
Copper (Cu), % 0
4.0 to 5.2
Iron (Fe), % 66.8 to 74.5
0 to 0.15
Magnesium (Mg), % 0
0.15 to 0.55
Manganese (Mn), % 0 to 2.0
0.2 to 0.5
Nickel (Ni), % 8.0 to 10.5
0
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.1
Silver (Ag), % 0
0.4 to 1.0
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0.15 to 0.35
Residuals, % 0
0 to 0.1

Comparable Variants