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SAE-AISI 4140 Steel vs. 3004 Aluminum

SAE-AISI 4140 steel belongs to the iron alloys classification, while 3004 aluminum belongs to the aluminum 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 SAE-AISI 4140 steel and the bottom bar is 3004 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 310
45 to 83
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 11 to 26
1.1 to 19
Fatigue Strength, MPa 360 to 650
55 to 120
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
26
Shear Strength, MPa 410 to 660
100 to 180
Tensile Strength: Ultimate (UTS), MPa 690 to 1080
170 to 310
Tensile Strength: Yield (Proof), MPa 590 to 990
68 to 270

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 420
180
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1420
630
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 43
160
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
42
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
140

Otherwise Unclassified Properties

Base Metal Price, % relative 2.4
9.5
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 1.5
8.3
Embodied Energy, MJ/kg 20
150
Embodied Water, L/kg 51
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 180
3.2 to 27
Resilience: Unit (Modulus of Resilience), kJ/m3 920 to 2590
33 to 540
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25 to 38
18 to 31
Strength to Weight: Bending, points 22 to 30
25 to 37
Thermal Diffusivity, mm2/s 12
65
Thermal Shock Resistance, points 20 to 32
7.6 to 13

Alloy Composition


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Aluminum (Al), % 0
95.6 to 98.2
Carbon (C), % 0.38 to 0.43
0
Chromium (Cr), % 0.8 to 1.1
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 96.8 to 97.8
0 to 0.7
Magnesium (Mg), % 0
0.8 to 1.3
Manganese (Mn), % 0.75 to 1.0
1.0 to 1.5
Molybdenum (Mo), % 0.15 to 0.25
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0.15 to 0.35
0 to 0.3
Sulfur (S), % 0 to 0.040
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants