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AISI 301L Stainless Steel vs. 852.0 Aluminum

AISI 301L stainless steel belongs to the iron alloys classification, while 852.0 aluminum belongs to the aluminum 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 AISI 301L stainless steel and the bottom bar is 852.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 320
64
Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 22 to 50
3.4
Fatigue Strength, MPa 240 to 530
73
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 440 to 660
130
Tensile Strength: Ultimate (UTS), MPa 620 to 1040
200
Tensile Strength: Yield (Proof), MPa 250 to 790
150

Thermal Properties

Latent Heat of Fusion, J/g 280
370
Maximum Temperature: Mechanical, °C 890
190
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1390
210
Specific Heat Capacity, J/kg-K 480
840
Thermal Conductivity, W/m-K 15
180
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
45
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
130

Otherwise Unclassified Properties

Base Metal Price, % relative 13
15
Density, g/cm3 7.8
3.2
Embodied Carbon, kg CO2/kg material 2.7
8.5
Embodied Energy, MJ/kg 39
160
Embodied Water, L/kg 130
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210 to 300
6.2
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 1580
160
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 25
43
Strength to Weight: Axial, points 22 to 37
17
Strength to Weight: Bending, points 21 to 29
24
Thermal Diffusivity, mm2/s 4.1
65
Thermal Shock Resistance, points 14 to 24
8.7

Alloy Composition

Aluminum (Al), % 0
86.6 to 91.3
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0
Copper (Cu), % 0
1.7 to 2.3
Iron (Fe), % 70.7 to 78
0 to 0.7
Magnesium (Mg), % 0
0.6 to 0.9
Manganese (Mn), % 0 to 2.0
0 to 0.1
Nickel (Ni), % 6.0 to 8.0
0.9 to 1.5
Nitrogen (N), % 0 to 0.2
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.030
0
Tin (Sn), % 0
5.5 to 7.0
Titanium (Ti), % 0
0 to 0.2
Residuals, % 0
0 to 0.3