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5154A Aluminum vs. SAE-AISI 9310 Steel

5154A aluminum belongs to the aluminum alloys classification, while SAE-AISI 9310 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 5154A aluminum and the bottom bar is SAE-AISI 9310 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 100
540 to 610
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.1 to 19
17 to 19
Fatigue Strength, MPa 83 to 160
300 to 390
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 140 to 210
510 to 570
Tensile Strength: Ultimate (UTS), MPa 230 to 370
820 to 910
Tensile Strength: Yield (Proof), MPa 96 to 320
450 to 570

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 190
440
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 600
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
48
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 110
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.4
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.8
1.8
Embodied Energy, MJ/kg 150
24
Embodied Water, L/kg 1180
57

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 36
120 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 760
540 to 860
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 24 to 38
29 to 32
Strength to Weight: Bending, points 31 to 43
25 to 27
Thermal Diffusivity, mm2/s 53
13
Thermal Shock Resistance, points 10 to 16
24 to 27

Alloy Composition

Aluminum (Al), % 93.7 to 96.9
0
Carbon (C), % 0
0.080 to 0.13
Chromium (Cr), % 0 to 0.25
1.0 to 1.4
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
93.8 to 95.2
Magnesium (Mg), % 3.1 to 3.9
0
Manganese (Mn), % 0 to 0.5
0.45 to 0.65
Molybdenum (Mo), % 0
0.080 to 0.15
Nickel (Ni), % 0
3.0 to 3.5
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.5
0.2 to 0.35
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants