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333.0 Aluminum vs. EN 1.4594 Stainless Steel

333.0 aluminum belongs to the aluminum alloys classification, while EN 1.4594 stainless steel belongs to the iron 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 333.0 aluminum and the bottom bar is EN 1.4594 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
200
Elongation at Break, % 1.0 to 2.0
11 to 17
Fatigue Strength, MPa 83 to 100
490 to 620
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 28
76
Shear Strength, MPa 190 to 230
620 to 700
Tensile Strength: Ultimate (UTS), MPa 230 to 280
1020 to 1170
Tensile Strength: Yield (Proof), MPa 130 to 210
810 to 1140

Thermal Properties

Latent Heat of Fusion, J/g 520
280
Maximum Temperature: Mechanical, °C 170
820
Melting Completion (Liquidus), °C 590
1450
Melting Onset (Solidus), °C 530
1410
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 100 to 140
16
Thermal Expansion, µm/m-K 21
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
15
Density, g/cm3 2.8
7.9
Embodied Carbon, kg CO2/kg material 7.6
3.2
Embodied Energy, MJ/kg 140
45
Embodied Water, L/kg 1040
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
110 to 190
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
1660 to 3320
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 22 to 27
36 to 41
Strength to Weight: Bending, points 29 to 34
29 to 31
Thermal Diffusivity, mm2/s 42 to 57
4.4
Thermal Shock Resistance, points 11 to 13
34 to 39

Alloy Composition

Aluminum (Al), % 81.8 to 89
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
13 to 15
Copper (Cu), % 3.0 to 4.0
1.2 to 2.0
Iron (Fe), % 0 to 1.0
72.6 to 79.5
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0 to 1.0
Molybdenum (Mo), % 0
1.2 to 2.0
Nickel (Ni), % 0 to 0.5
5.0 to 6.0
Niobium (Nb), % 0
0.15 to 0.6
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 8.0 to 10
0 to 0.7
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0