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AISI 316L Stainless Steel vs. 2025 Aluminum

AISI 316L stainless steel belongs to the iron alloys classification, while 2025 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 AISI 316L stainless steel and the bottom bar is 2025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 350
110
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 9.0 to 50
15
Fatigue Strength, MPa 170 to 450
130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
27
Shear Strength, MPa 370 to 690
240
Tensile Strength: Ultimate (UTS), MPa 530 to 1160
400
Tensile Strength: Yield (Proof), MPa 190 to 870
260

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 870
190
Melting Completion (Liquidus), °C 1400
640
Melting Onset (Solidus), °C 1380
520
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 15
150
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
120

Otherwise Unclassified Properties

Base Metal Price, % relative 19
10
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 3.9
7.9
Embodied Energy, MJ/kg 53
150
Embodied Water, L/kg 150
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 77 to 230
55
Resilience: Unit (Modulus of Resilience), kJ/m3 93 to 1880
450
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 19 to 41
37
Strength to Weight: Bending, points 18 to 31
40
Thermal Diffusivity, mm2/s 4.1
58
Thermal Shock Resistance, points 12 to 25
18

Alloy Composition

Aluminum (Al), % 0
90.9 to 95.2
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0 to 0.1
Copper (Cu), % 0
3.9 to 5.0
Iron (Fe), % 62 to 72
0 to 1.0
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0 to 2.0
0.4 to 1.2
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 10 to 14
0
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0.5 to 1.2
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15