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EN 1.4567 Stainless Steel vs. 518.0 Aluminum

EN 1.4567 stainless steel belongs to the iron alloys classification, while 518.0 aluminum belongs to the aluminum 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 EN 1.4567 stainless steel and the bottom bar is 518.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 240
80
Elastic (Young's, Tensile) Modulus, GPa 190
67
Elongation at Break, % 22 to 51
5.0
Fatigue Strength, MPa 190 to 260
140
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
25
Shear Strength, MPa 390 to 490
200
Tensile Strength: Ultimate (UTS), MPa 550 to 780
310
Tensile Strength: Yield (Proof), MPa 200 to 390
190

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 930
170
Melting Completion (Liquidus), °C 1410
620
Melting Onset (Solidus), °C 1370
560
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 11
98
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
24
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
81

Otherwise Unclassified Properties

Base Metal Price, % relative 16
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.1
9.4
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 150
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 220
14
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 400
270
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 19 to 27
32
Strength to Weight: Bending, points 19 to 24
38
Thermal Diffusivity, mm2/s 3.0
40
Thermal Shock Resistance, points 12 to 17
14

Alloy Composition

Aluminum (Al), % 0
88.1 to 92.5
Carbon (C), % 0 to 0.040
0
Chromium (Cr), % 17 to 19
0
Copper (Cu), % 3.0 to 4.0
0 to 0.25
Iron (Fe), % 63.3 to 71.5
0 to 1.8
Magnesium (Mg), % 0
7.5 to 8.5
Manganese (Mn), % 0 to 2.0
0 to 0.35
Nickel (Ni), % 8.5 to 10.5
0 to 0.15
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.35
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.25