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AISI 301LN Stainless Steel vs. 5454 Aluminum

AISI 301LN stainless steel belongs to the iron alloys classification, while 5454 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 301LN stainless steel and the bottom bar is 5454 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 320
61 to 93
Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 23 to 51
2.3 to 18
Fatigue Strength, MPa 270 to 520
83 to 160
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 450 to 670
140 to 200
Tensile Strength: Ultimate (UTS), MPa 630 to 1060
230 to 350
Tensile Strength: Yield (Proof), MPa 270 to 770
97 to 290

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 890
190
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1380
600
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 15
130
Thermal Expansion, µm/m-K 16
24

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 13
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.6
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 220 to 290
6.3 to 34
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 1520
68 to 590
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 22 to 38
23 to 36
Strength to Weight: Bending, points 21 to 30
30 to 41
Thermal Diffusivity, mm2/s 4.0
55
Thermal Shock Resistance, points 14 to 24
10 to 16

Alloy Composition

Aluminum (Al), % 0
94.5 to 97.1
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0.050 to 0.2
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 70.7 to 77.9
0 to 0.4
Magnesium (Mg), % 0
2.4 to 3.0
Manganese (Mn), % 0 to 2.0
0.5 to 1.0
Nickel (Ni), % 6.0 to 8.0
0
Nitrogen (N), % 0.070 to 0.2
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.25
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants