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AISI 310S Stainless Steel vs. EN AC-46400 Aluminum

AISI 310S stainless steel belongs to the iron alloys classification, while EN AC-46400 aluminum belongs to the aluminum alloys. There are 30 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 310S stainless steel and the bottom bar is EN AC-46400 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 210
77 to 120
Elastic (Young's, Tensile) Modulus, GPa 200
72
Elongation at Break, % 34 to 44
1.1 to 1.7
Fatigue Strength, MPa 250 to 280
75 to 85
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 79
27
Tensile Strength: Ultimate (UTS), MPa 600 to 710
170 to 310
Tensile Strength: Yield (Proof), MPa 270 to 350
110 to 270

Thermal Properties

Latent Heat of Fusion, J/g 310
520
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1450
610
Melting Onset (Solidus), °C 1400
570
Specific Heat Capacity, J/kg-K 480
890
Thermal Conductivity, W/m-K 16
130
Thermal Expansion, µm/m-K 16
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.0
33
Electrical Conductivity: Equal Weight (Specific), % IACS 2.3
110

Otherwise Unclassified Properties

Base Metal Price, % relative 25
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 4.3
7.8
Embodied Energy, MJ/kg 61
150
Embodied Water, L/kg 190
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 220
1.7 to 4.9
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 310
82 to 500
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
52
Strength to Weight: Axial, points 21 to 25
18 to 32
Strength to Weight: Bending, points 20 to 22
26 to 38
Thermal Diffusivity, mm2/s 4.1
55
Thermal Shock Resistance, points 14 to 16
7.8 to 14

Alloy Composition


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Aluminum (Al), % 0
85.4 to 90.5
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 24 to 26
0
Copper (Cu), % 0
0.8 to 1.3
Iron (Fe), % 48.3 to 57
0 to 0.8
Lead (Pb), % 0
0 to 0.1
Magnesium (Mg), % 0
0.25 to 0.65
Manganese (Mn), % 0 to 2.0
0.15 to 0.55
Nickel (Ni), % 19 to 22
0 to 0.2
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.5
8.3 to 9.7
Sulfur (S), % 0 to 0.030
0
Tin (Sn), % 0
0 to 0.1
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.8
Residuals, % 0
0 to 0.25