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5383 Aluminum vs. SAE-AISI 52100 Steel

5383 aluminum belongs to the aluminum alloys classification, while SAE-AISI 52100 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 5383 aluminum and the bottom bar is SAE-AISI 52100 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 110
180 to 210
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.7 to 15
10 to 20
Fatigue Strength, MPa 130 to 200
250 to 340
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 190 to 220
370 to 420
Tensile Strength: Ultimate (UTS), MPa 310 to 370
590 to 2010
Tensile Strength: Yield (Proof), MPa 150 to 310
360 to 560

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 200
430
Melting Completion (Liquidus), °C 650
1450
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
47
Thermal Expansion, µm/m-K 24
12 to 13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 97
8.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.4
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
1.5
Embodied Energy, MJ/kg 160
20
Embodied Water, L/kg 1170
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
54 to 310
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
350 to 840
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 32 to 38
21 to 72
Strength to Weight: Bending, points 38 to 42
20 to 45
Thermal Diffusivity, mm2/s 51
13
Thermal Shock Resistance, points 14 to 16
19 to 61

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0.93 to 1.1
Chromium (Cr), % 0 to 0.25
1.4 to 1.6
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.25
96.5 to 97.3
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
0.25 to 0.45
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.25
0.15 to 0.35
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants