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ASTM A387 Grade 21 Steel vs. 4004 Aluminum

ASTM A387 grade 21 steel belongs to the iron alloys classification, while 4004 aluminum belongs to the aluminum 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 ASTM A387 grade 21 steel and the bottom bar is 4004 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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