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AISI 201L Stainless Steel vs. 1080A Aluminum

AISI 201L stainless steel belongs to the iron alloys classification, while 1080A aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 AISI 201L stainless steel and the bottom bar is 1080A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190 to 320
18 to 40
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 22 to 46
2.3 to 34
Fatigue Strength, MPa 270 to 530
18 to 50
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 520 to 660
49 to 81
Tensile Strength: Ultimate (UTS), MPa 740 to 1040
74 to 140
Tensile Strength: Yield (Proof), MPa 290 to 790
17 to 120

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 880
170
Melting Completion (Liquidus), °C 1410
640
Melting Onset (Solidus), °C 1370
640
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 15
230
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
62
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
200

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 2.6
8.3
Embodied Energy, MJ/kg 38
160
Embodied Water, L/kg 140
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210 to 300
3.1 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 1570
2.1 to 100
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 27 to 37
7.6 to 15
Strength to Weight: Bending, points 24 to 30
14 to 22
Thermal Diffusivity, mm2/s 4.0
94
Thermal Shock Resistance, points 16 to 23
3.3 to 6.4

Alloy Composition

Aluminum (Al), % 0
99.8 to 100
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0
Copper (Cu), % 0
0 to 0.030
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 67.9 to 75
0 to 0.15
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 5.5 to 7.5
0 to 0.020
Nickel (Ni), % 3.5 to 5.5
0
Nitrogen (N), % 0 to 0.25
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0 to 0.15
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.020
Zinc (Zn), % 0
0 to 0.060

Comparable Variants