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EN 1.4567 Stainless Steel vs. 360.0 Aluminum

EN 1.4567 stainless steel belongs to the iron alloys classification, while 360.0 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 360.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 240
75
Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 22 to 51
2.5
Fatigue Strength, MPa 190 to 260
140
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 390 to 490
190
Tensile Strength: Ultimate (UTS), MPa 550 to 780
300
Tensile Strength: Yield (Proof), MPa 200 to 390
170

Thermal Properties

Latent Heat of Fusion, J/g 290
530
Maximum Temperature: Mechanical, °C 930
170
Melting Completion (Liquidus), °C 1410
590
Melting Onset (Solidus), °C 1370
570
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 11
130
Thermal Expansion, µm/m-K 17
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
110

Otherwise Unclassified Properties

Base Metal Price, % relative 16
9.5
Density, g/cm3 7.8
2.6
Embodied Carbon, kg CO2/kg material 3.1
7.8
Embodied Energy, MJ/kg 43
140
Embodied Water, L/kg 150
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 220
6.4
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 400
200
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
53
Strength to Weight: Axial, points 19 to 27
32
Strength to Weight: Bending, points 19 to 24
38
Thermal Diffusivity, mm2/s 3.0
55
Thermal Shock Resistance, points 12 to 17
14

Alloy Composition


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Aluminum (Al), % 0
85.1 to 90.6
Carbon (C), % 0 to 0.040
0
Chromium (Cr), % 17 to 19
0
Copper (Cu), % 3.0 to 4.0
0 to 0.6
Iron (Fe), % 63.3 to 71.5
0 to 2.0
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0 to 2.0
0 to 0.35
Nickel (Ni), % 8.5 to 10.5
0 to 0.5
Nitrogen (N), % 0 to 0.1
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
9.0 to 10
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25