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242.0 Aluminum vs. SAE-AISI 4340M Steel

242.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340M steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (6, 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 242.0 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 70 to 110
710
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 0.5 to 1.5
6.0
Fatigue Strength, MPa 55 to 110
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
72
Shear Strength, MPa 150 to 240
1360
Tensile Strength: Ultimate (UTS), MPa 180 to 290
2340
Tensile Strength: Yield (Proof), MPa 120 to 220
1240

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Mechanical, °C 210
430
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 530
1400
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 130 to 170
38
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 44
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 96 to 130
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 12
3.9
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1130
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 3.4
120
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 340
4120
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 16 to 26
84
Strength to Weight: Bending, points 23 to 32
51
Thermal Diffusivity, mm2/s 50 to 62
10
Thermal Shock Resistance, points 8.0 to 13
70

Alloy Composition

Aluminum (Al), % 88.4 to 93.6
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0 to 0.25
0.7 to 1.0
Copper (Cu), % 3.5 to 4.5
0
Iron (Fe), % 0 to 1.0
93.3 to 94.8
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.35
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 1.7 to 2.3
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 0 to 0.7
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0