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AISI 310 Stainless Steel vs. 852.0 Aluminum

AISI 310 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 (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 310 stainless steel and the bottom bar is 852.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 180 to 220
64
Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 34 to 45
3.4
Fatigue Strength, MPa 240 to 280
73
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 78
26
Shear Strength, MPa 420 to 470
130
Tensile Strength: Ultimate (UTS), MPa 600 to 710
200
Tensile Strength: Yield (Proof), MPa 260 to 350
150

Thermal Properties

Latent Heat of Fusion, J/g 310
370
Maximum Temperature: Mechanical, °C 1040
190
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1400
210
Specific Heat Capacity, J/kg-K 480
840
Thermal Conductivity, W/m-K 15
180
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
45
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
130

Otherwise Unclassified Properties

Base Metal Price, % relative 25
15
Density, g/cm3 7.8
3.2
Embodied Carbon, kg CO2/kg material 4.3
8.5
Embodied Energy, MJ/kg 61
160
Embodied Water, L/kg 190
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 220
6.2
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 310
160
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 25
43
Strength to Weight: Axial, points 21 to 25
17
Strength to Weight: Bending, points 20 to 22
24
Thermal Diffusivity, mm2/s 3.9
65
Thermal Shock Resistance, points 14 to 17
8.7

Alloy Composition

Aluminum (Al), % 0
86.6 to 91.3
Carbon (C), % 0 to 0.25
0
Chromium (Cr), % 24 to 26
0
Copper (Cu), % 0
1.7 to 2.3
Iron (Fe), % 48.2 to 57
0 to 0.7
Magnesium (Mg), % 0
0.6 to 0.9
Manganese (Mn), % 0 to 2.0
0 to 0.1
Nickel (Ni), % 19 to 22
0.9 to 1.5
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.5
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