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1080A Aluminum vs. EN 1.4659 Stainless Steel

1080A aluminum belongs to the aluminum alloys classification, while EN 1.4659 stainless steel belongs to the iron 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 1080A aluminum and the bottom bar is EN 1.4659 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 18 to 40
260
Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 2.3 to 34
49
Fatigue Strength, MPa 18 to 50
460
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 49 to 81
640
Tensile Strength: Ultimate (UTS), MPa 74 to 140
900
Tensile Strength: Yield (Proof), MPa 17 to 120
480

Thermal Properties

Latent Heat of Fusion, J/g 400
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 640
1480
Melting Onset (Solidus), °C 640
1430
Specific Heat Capacity, J/kg-K 900
460
Thermal Conductivity, W/m-K 230
12
Thermal Expansion, µm/m-K 23
16

Electrical Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
37
Density, g/cm3 2.7
8.2
Embodied Carbon, kg CO2/kg material 8.3
6.5
Embodied Energy, MJ/kg 160
89
Embodied Water, L/kg 1200
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.1 to 19
370
Resilience: Unit (Modulus of Resilience), kJ/m3 2.1 to 100
550
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.6 to 15
31
Strength to Weight: Bending, points 14 to 22
25
Thermal Diffusivity, mm2/s 94
3.2
Thermal Shock Resistance, points 3.3 to 6.4
19

Alloy Composition

Aluminum (Al), % 99.8 to 100
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0
23 to 25
Copper (Cu), % 0 to 0.030
1.0 to 2.0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.15
35.7 to 45.7
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0 to 0.020
2.0 to 4.0
Molybdenum (Mo), % 0
5.5 to 6.5
Nickel (Ni), % 0
21 to 23
Nitrogen (N), % 0
0.35 to 0.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.15
0 to 0.7
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.020
0
Tungsten (W), % 0
1.5 to 2.5
Zinc (Zn), % 0 to 0.060
0