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5252 Aluminum vs. EN 1.4913 Stainless Steel

5252 aluminum belongs to the aluminum alloys classification, while EN 1.4913 stainless steel belongs to the iron 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 5252 aluminum and the bottom bar is EN 1.4913 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 4.5 to 11
14 to 22
Fatigue Strength, MPa 100 to 110
320 to 480
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
75
Shear Strength, MPa 140 to 160
550 to 590
Tensile Strength: Ultimate (UTS), MPa 230 to 290
870 to 980
Tensile Strength: Yield (Proof), MPa 170 to 240
480 to 850

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 180
700
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 610
1410
Specific Heat Capacity, J/kg-K 910
480
Thermal Conductivity, W/m-K 140
24
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 120
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.0
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.7
2.9
Embodied Energy, MJ/kg 160
41
Embodied Water, L/kg 1190
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 23
130 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 430
600 to 1860
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 23 to 30
31 to 35
Strength to Weight: Bending, points 31 to 36
26 to 28
Thermal Diffusivity, mm2/s 57
6.5
Thermal Shock Resistance, points 10 to 13
31 to 34

Alloy Composition


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Aluminum (Al), % 96.6 to 97.8
0 to 0.020
Boron (B), % 0
0 to 0.0015
Carbon (C), % 0
0.17 to 0.23
Chromium (Cr), % 0
10 to 11.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.1
84.5 to 88.3
Magnesium (Mg), % 2.2 to 2.8
0
Manganese (Mn), % 0 to 0.1
0.4 to 0.9
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0
0.2 to 0.6
Niobium (Nb), % 0
0.25 to 0.55
Nitrogen (N), % 0
0.050 to 0.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.080
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0 to 0.050
0.1 to 0.3
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0