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EN 1.4371 Stainless Steel vs. 2030 Aluminum

EN 1.4371 stainless steel belongs to the iron alloys classification, while 2030 aluminum belongs to the aluminum alloys. There are 30 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 1.4371 stainless steel and the bottom bar is 2030 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 45 to 51
5.6 to 8.0
Fatigue Strength, MPa 290 to 340
91 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 520 to 540
220 to 250
Tensile Strength: Ultimate (UTS), MPa 740 to 750
370 to 420
Tensile Strength: Yield (Proof), MPa 320 to 340
240 to 270

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Mechanical, °C 880
190
Melting Completion (Liquidus), °C 1410
640
Melting Onset (Solidus), °C 1370
510
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 15
130
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
99

Otherwise Unclassified Properties

Base Metal Price, % relative 12
10
Density, g/cm3 7.7
3.1
Embodied Carbon, kg CO2/kg material 2.6
8.0
Embodied Energy, MJ/kg 38
150
Embodied Water, L/kg 140
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 270 to 310
21 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 300
390 to 530
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 27
33 to 38
Strength to Weight: Bending, points 24
37 to 40
Thermal Diffusivity, mm2/s 4.0
50
Thermal Shock Resistance, points 16
16 to 19

Alloy Composition

Aluminum (Al), % 0
88.9 to 95.2
Bismuth (Bi), % 0
0 to 0.2
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 17.5
0 to 0.1
Copper (Cu), % 0 to 1.0
3.3 to 4.5
Iron (Fe), % 66.7 to 74.4
0 to 0.7
Lead (Pb), % 0
0.8 to 1.5
Magnesium (Mg), % 0
0.5 to 1.3
Manganese (Mn), % 6.0 to 8.0
0.2 to 1.0
Nickel (Ni), % 3.5 to 5.5
0
Nitrogen (N), % 0.15 to 0.25
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.8
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.3