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EN 1.4859 Stainless Steel vs. 333.0 Aluminum

EN 1.4859 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 (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 EN 1.4859 stainless steel and the bottom bar is 333.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140
90 to 110
Elastic (Young's, Tensile) Modulus, GPa 200
73
Elongation at Break, % 23
1.0 to 2.0
Fatigue Strength, MPa 140
83 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
28
Tensile Strength: Ultimate (UTS), MPa 490
230 to 280
Tensile Strength: Yield (Proof), MPa 210
130 to 210

Thermal Properties

Latent Heat of Fusion, J/g 310
520
Maximum Temperature: Mechanical, °C 1050
170
Melting Completion (Liquidus), °C 1410
590
Melting Onset (Solidus), °C 1360
530
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 13
100 to 140
Thermal Expansion, µm/m-K 16
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
26 to 35
Electrical Conductivity: Equal Weight (Specific), % IACS 1.9
83 to 110

Otherwise Unclassified Properties

Base Metal Price, % relative 36
10
Density, g/cm3 8.0
2.8
Embodied Carbon, kg CO2/kg material 6.2
7.6
Embodied Energy, MJ/kg 88
140
Embodied Water, L/kg 190
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 91
2.1 to 4.6
Resilience: Unit (Modulus of Resilience), kJ/m3 110
120 to 290
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
49
Strength to Weight: Axial, points 17
22 to 27
Strength to Weight: Bending, points 17
29 to 34
Thermal Diffusivity, mm2/s 3.4
42 to 57
Thermal Shock Resistance, points 11
11 to 13

Alloy Composition

Aluminum (Al), % 0
81.8 to 89
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 19 to 21
0
Copper (Cu), % 0
3.0 to 4.0
Iron (Fe), % 40.3 to 49
0 to 1.0
Magnesium (Mg), % 0
0.050 to 0.5
Manganese (Mn), % 0 to 2.0
0 to 0.5
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 31 to 33
0 to 0.5
Niobium (Nb), % 0.5 to 1.5
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0.5 to 1.5
8.0 to 10
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5