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SAE-AISI 4340M Steel vs. 3103 Aluminum

SAE-AISI 4340M steel belongs to the iron alloys classification, while 3103 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 3103 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 710
27 to 62
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 6.0
1.1 to 28
Fatigue Strength, MPa 690
38 to 83
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 1360
68 to 130
Tensile Strength: Ultimate (UTS), MPa 2340
100 to 220
Tensile Strength: Yield (Proof), MPa 1240
39 to 200

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 430
190
Melting Completion (Liquidus), °C 1440
660
Melting Onset (Solidus), °C 1400
640
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 38
160
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
42
Electrical Conductivity: Equal Weight (Specific), % IACS 9.1
140

Otherwise Unclassified Properties

Base Metal Price, % relative 3.9
9.5
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 1.9
8.2
Embodied Energy, MJ/kg 26
150
Embodied Water, L/kg 55
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
2.4 to 24
Resilience: Unit (Modulus of Resilience), kJ/m3 4120
11 to 280
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 84
10 to 22
Strength to Weight: Bending, points 51
18 to 30
Thermal Diffusivity, mm2/s 10
64
Thermal Shock Resistance, points 70
4.6 to 9.9

Alloy Composition

Aluminum (Al), % 0
96.3 to 99.1
Carbon (C), % 0.38 to 0.43
0
Chromium (Cr), % 0.7 to 1.0
0 to 0.1
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 93.3 to 94.8
0 to 0.7
Magnesium (Mg), % 0
0 to 0.3
Manganese (Mn), % 0.65 to 0.9
0.9 to 1.5
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 0.5
Sulfur (S), % 0 to 0.012
0
Titanium (Ti), % 0
0 to 0.1
Vanadium (V), % 0.050 to 0.1
0
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0 to 0.1
Residuals, % 0
0 to 0.15