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A360.0 Aluminum vs. S33425 Stainless Steel

A360.0 aluminum belongs to the aluminum alloys classification, while S33425 stainless steel belongs to the iron 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 A360.0 aluminum and the bottom bar is S33425 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
170
Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 1.6 to 5.0
45
Fatigue Strength, MPa 82 to 150
210
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
79
Shear Strength, MPa 180
400
Tensile Strength: Ultimate (UTS), MPa 180 to 320
580
Tensile Strength: Yield (Proof), MPa 170 to 260
230

Thermal Properties

Latent Heat of Fusion, J/g 530
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 680
1430
Melting Onset (Solidus), °C 590
1380
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 110
14
Thermal Expansion, µm/m-K 21
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
2.1
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
27
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 7.8
5.1
Embodied Energy, MJ/kg 150
71
Embodied Water, L/kg 1070
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 13
210
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 470
140
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 19 to 34
20
Strength to Weight: Bending, points 27 to 39
19
Thermal Diffusivity, mm2/s 48
3.7
Thermal Shock Resistance, points 8.5 to 15
13

Alloy Composition

Aluminum (Al), % 85.8 to 90.6
0.15 to 0.6
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
21 to 23
Copper (Cu), % 0 to 0.6
0
Iron (Fe), % 0 to 1.3
47.2 to 56.7
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.35
0 to 1.5
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0 to 0.5
20 to 23
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 9.0 to 10
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0
0.15 to 0.6
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.25
0