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SAE-AISI 4340M Steel vs. 5005 Aluminum

SAE-AISI 4340M steel belongs to the iron alloys classification, while 5005 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 SAE-AISI 4340M steel and the bottom bar is 5005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 710
28 to 64
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 6.0
1.1 to 23
Fatigue Strength, MPa 690
38 to 86
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 1360
70 to 130
Tensile Strength: Ultimate (UTS), MPa 2340
110 to 230
Tensile Strength: Yield (Proof), MPa 1240
41 to 210

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 430
180
Melting Completion (Liquidus), °C 1440
650
Melting Onset (Solidus), °C 1400
630
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 38
200
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
52
Electrical Conductivity: Equal Weight (Specific), % IACS 9.1
170

Otherwise Unclassified Properties

Base Metal Price, % relative 3.9
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.9
8.3
Embodied Energy, MJ/kg 26
150
Embodied Water, L/kg 55
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
2.3 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 4120
12 to 320
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 84
11 to 23
Strength to Weight: Bending, points 51
19 to 31
Thermal Diffusivity, mm2/s 10
82
Thermal Shock Resistance, points 70
4.9 to 10

Alloy Composition

Aluminum (Al), % 0
97 to 99.5
Carbon (C), % 0.38 to 0.43
0
Chromium (Cr), % 0.7 to 1.0
0 to 0.1
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 93.3 to 94.8
0 to 0.7
Magnesium (Mg), % 0
0.5 to 1.1
Manganese (Mn), % 0.65 to 0.9
0 to 0.2
Molybdenum (Mo), % 0.35 to 0.45
0
Nickel (Ni), % 1.7 to 2.0
0
Phosphorus (P), % 0 to 0.012
0
Silicon (Si), % 1.5 to 1.8
0 to 0.3
Sulfur (S), % 0 to 0.012
0
Vanadium (V), % 0.050 to 0.1
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15