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A360.0 Aluminum vs. S44800 Stainless Steel

A360.0 aluminum belongs to the aluminum alloys classification, while S44800 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 A360.0 aluminum and the bottom bar is S44800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
190
Elastic (Young's, Tensile) Modulus, GPa 72
210
Elongation at Break, % 1.6 to 5.0
23
Fatigue Strength, MPa 82 to 150
300
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 27
82
Shear Strength, MPa 180
370
Tensile Strength: Ultimate (UTS), MPa 180 to 320
590
Tensile Strength: Yield (Proof), MPa 170 to 260
450

Thermal Properties

Latent Heat of Fusion, J/g 530
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 680
1460
Melting Onset (Solidus), °C 590
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 110
17
Thermal Expansion, µm/m-K 21
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
19
Density, g/cm3 2.6
7.8
Embodied Carbon, kg CO2/kg material 7.8
3.8
Embodied Energy, MJ/kg 150
52
Embodied Water, L/kg 1070
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 13
120
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 470
480
Stiffness to Weight: Axial, points 15
15
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 19 to 34
21
Strength to Weight: Bending, points 27 to 39
20
Thermal Diffusivity, mm2/s 48
4.6
Thermal Shock Resistance, points 8.5 to 15
19

Alloy Composition

Aluminum (Al), % 85.8 to 90.6
0
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0
28 to 30
Copper (Cu), % 0 to 0.6
0 to 0.15
Iron (Fe), % 0 to 1.3
62.6 to 66.5
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.35
0 to 0.3
Molybdenum (Mo), % 0
3.5 to 4.2
Nickel (Ni), % 0 to 0.5
2.0 to 2.5
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 9.0 to 10
0 to 0.2
Sulfur (S), % 0
0 to 0.020
Tin (Sn), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.25
0