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4004 Aluminum vs. ASTM A387 Grade 21 Steel

4004 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 21 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 4004 aluminum and the bottom bar is ASTM A387 grade 21 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 2.4
21
Fatigue Strength, MPa 42
160 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Shear Strength, MPa 63
310 to 370
Tensile Strength: Ultimate (UTS), MPa 110
500 to 590
Tensile Strength: Yield (Proof), MPa 60
230 to 350

Thermal Properties

Latent Heat of Fusion, J/g 540
260
Maximum Temperature: Mechanical, °C 160
480
Melting Completion (Liquidus), °C 600
1470
Melting Onset (Solidus), °C 560
1430
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 130
41
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.1
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 8.0
1.8
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1070
62

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3
84 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 25
140 to 320
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 54
24
Strength to Weight: Axial, points 12
18 to 21
Strength to Weight: Bending, points 20
18 to 20
Thermal Diffusivity, mm2/s 58
11
Thermal Shock Resistance, points 5.1
14 to 17

Alloy Composition

Aluminum (Al), % 86 to 90
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
2.8 to 3.3
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.8
94.4 to 96
Magnesium (Mg), % 1.0 to 2.0
0
Manganese (Mn), % 0 to 0.1
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 9.0 to 10.5
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0