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5252 Aluminum vs. S35115 Stainless Steel

5252 aluminum belongs to the aluminum alloys classification, while S35115 stainless steel belongs to the iron alloys. There are 31 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 S35115 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 68 to 75
210
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 4.5 to 11
46
Fatigue Strength, MPa 100 to 110
280
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
79
Shear Strength, MPa 140 to 160
470
Tensile Strength: Ultimate (UTS), MPa 230 to 290
670
Tensile Strength: Yield (Proof), MPa 170 to 240
310

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 650
1420
Melting Onset (Solidus), °C 610
1370
Specific Heat Capacity, J/kg-K 910
480
Thermal Conductivity, W/m-K 140
15
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
26
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.7
4.8
Embodied Energy, MJ/kg 160
67
Embodied Water, L/kg 1190
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 23
250
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 430
240
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 23 to 30
24
Strength to Weight: Bending, points 31 to 36
22
Thermal Diffusivity, mm2/s 57
3.9
Thermal Shock Resistance, points 10 to 13
15

Alloy Composition

Aluminum (Al), % 96.6 to 97.8
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
23 to 25
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.1
47.6 to 55.8
Magnesium (Mg), % 2.2 to 2.8
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Molybdenum (Mo), % 0
1.5 to 2.5
Nickel (Ni), % 0
19 to 22
Nitrogen (N), % 0
0.2 to 0.3
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.080
0.5 to 1.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0