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3003 Aluminum vs. SAE-AISI 4340M Steel

3003 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 (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 3003 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 28 to 65
710
Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 1.1 to 28
6.0
Fatigue Strength, MPa 39 to 90
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 68 to 130
1360
Tensile Strength: Ultimate (UTS), MPa 110 to 240
2340
Tensile Strength: Yield (Proof), MPa 40 to 210
1240

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 180
430
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 640
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 180
38
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 44
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 140
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.9
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.1
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1180
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.95 to 63
120
Resilience: Unit (Modulus of Resilience), kJ/m3 11 to 300
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 11 to 24
84
Strength to Weight: Bending, points 18 to 30
51
Thermal Diffusivity, mm2/s 71
10
Thermal Shock Resistance, points 4.7 to 10
70

Alloy Composition


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Aluminum (Al), % 96.8 to 99
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0
0.7 to 1.0
Copper (Cu), % 0.050 to 0.2
0
Iron (Fe), % 0 to 0.7
93.3 to 94.8
Manganese (Mn), % 1.0 to 1.5
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 0
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 0 to 0.6
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0