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1350 Aluminum vs. EN 1.4865 Stainless Steel

1350 aluminum belongs to the aluminum alloys classification, while EN 1.4865 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 1350 aluminum and the bottom bar is EN 1.4865 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 20 to 45
140
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.4 to 30
6.8
Fatigue Strength, MPa 24 to 50
120
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 68 to 190
470
Tensile Strength: Yield (Proof), MPa 25 to 170
250

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 170
1020
Melting Completion (Liquidus), °C 660
1380
Melting Onset (Solidus), °C 650
1330
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 230
12
Thermal Expansion, µm/m-K 24
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
33
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.3
5.8
Embodied Energy, MJ/kg 160
81
Embodied Water, L/kg 1200
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
27
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.0 to 19
16
Strength to Weight: Bending, points 14 to 27
17
Thermal Diffusivity, mm2/s 96
3.1
Thermal Shock Resistance, points 3.0 to 8.2
11

Alloy Composition

Aluminum (Al), % 99.5 to 100
0
Boron (B), % 0 to 0.050
0
Carbon (C), % 0
0.3 to 0.5
Chromium (Cr), % 0 to 0.010
18 to 21
Copper (Cu), % 0 to 0.050
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
34.4 to 44.7
Manganese (Mn), % 0 to 0.010
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
36 to 39
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
1.0 to 2.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.020
0
Vanadium (V), % 0 to 0.020
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0