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AISI 310S Stainless Steel vs. 2025 Aluminum

AISI 310S 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 (2, 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 310S stainless steel and the bottom bar is 2025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 210
110
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 34 to 44
15
Fatigue Strength, MPa 250 to 280
130
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 79
27
Shear Strength, MPa 420 to 470
240
Tensile Strength: Ultimate (UTS), MPa 600 to 710
400
Tensile Strength: Yield (Proof), MPa 270 to 350
260

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 1100
190
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1400
520
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 16
150
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.0
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.3
120

Otherwise Unclassified Properties

Base Metal Price, % relative 25
10
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 4.3
7.9
Embodied Energy, MJ/kg 61
150
Embodied Water, L/kg 190
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 220
55
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 310
450
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 21 to 25
37
Strength to Weight: Bending, points 20 to 22
40
Thermal Diffusivity, mm2/s 4.1
58
Thermal Shock Resistance, points 14 to 16
18

Alloy Composition


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Aluminum (Al), % 0
90.9 to 95.2
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 24 to 26
0 to 0.1
Copper (Cu), % 0
3.9 to 5.0
Iron (Fe), % 48.3 to 57
0 to 1.0
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0 to 2.0
0.4 to 1.2
Nickel (Ni), % 19 to 22
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.5
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