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EN 1.4923 Stainless Steel vs. 333.0 Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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

Comparable Variants