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333.0 Aluminum vs. EN 1.4923 Stainless Steel

333.0 aluminum belongs to the aluminum alloys classification, while EN 1.4923 stainless steel belongs to the iron alloys. There are 30 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 333.0 aluminum and the bottom bar is EN 1.4923 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 1.0 to 2.0
12 to 21
Fatigue Strength, MPa 83 to 100
300 to 440
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 28
76
Shear Strength, MPa 190 to 230
540 to 590
Tensile Strength: Ultimate (UTS), MPa 230 to 280
870 to 980
Tensile Strength: Yield (Proof), MPa 130 to 210
470 to 780

Thermal Properties

Latent Heat of Fusion, J/g 520
270
Maximum Temperature: Mechanical, °C 170
740
Melting Completion (Liquidus), °C 590
1450
Melting Onset (Solidus), °C 530
1410
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 100 to 140
24
Thermal Expansion, µm/m-K 21
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
8.0
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 7.6
2.9
Embodied Energy, MJ/kg 140
41
Embodied Water, L/kg 1040
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
570 to 1580
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 22 to 27
31 to 35
Strength to Weight: Bending, points 29 to 34
26 to 28
Thermal Diffusivity, mm2/s 42 to 57
6.5
Thermal Shock Resistance, points 11 to 13
30 to 34

Alloy Composition


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Aluminum (Al), % 81.8 to 89
0
Carbon (C), % 0
0.18 to 0.24
Chromium (Cr), % 0
11 to 12.5
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 1.0
83.5 to 87.1
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0.4 to 0.9
Molybdenum (Mo), % 0
0.8 to 1.2
Nickel (Ni), % 0 to 0.5
0.3 to 0.8
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 8.0 to 10
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.25 to 0.35
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0

Comparable Variants