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333.0 Aluminum vs. S20433 Stainless Steel

333.0 aluminum belongs to the aluminum alloys classification, while S20433 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 333.0 aluminum and the bottom bar is S20433 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 90 to 110
190
Elastic (Young's, Tensile) Modulus, GPa 73
200
Elongation at Break, % 1.0 to 2.0
46
Fatigue Strength, MPa 83 to 100
250
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 28
76
Shear Strength, MPa 190 to 230
440
Tensile Strength: Ultimate (UTS), MPa 230 to 280
630
Tensile Strength: Yield (Proof), MPa 130 to 210
270

Thermal Properties

Latent Heat of Fusion, J/g 520
280
Maximum Temperature: Mechanical, °C 170
900
Melting Completion (Liquidus), °C 590
1400
Melting Onset (Solidus), °C 530
1360
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 100 to 140
15
Thermal Expansion, µm/m-K 21
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 10
13
Density, g/cm3 2.8
7.7
Embodied Carbon, kg CO2/kg material 7.6
2.7
Embodied Energy, MJ/kg 140
39
Embodied Water, L/kg 1040
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
230
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
180
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 22 to 27
23
Strength to Weight: Bending, points 29 to 34
21
Thermal Diffusivity, mm2/s 42 to 57
4.0
Thermal Shock Resistance, points 11 to 13
14

Alloy Composition

Aluminum (Al), % 81.8 to 89
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
17 to 18
Copper (Cu), % 3.0 to 4.0
1.5 to 3.5
Iron (Fe), % 0 to 1.0
64.1 to 72.4
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
5.5 to 7.5
Nickel (Ni), % 0 to 0.5
3.5 to 5.5
Nitrogen (N), % 0
0.1 to 0.25
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 8.0 to 10
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0