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2030 Aluminum vs. ASTM A387 Grade 2 Steel

2030 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 2 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 2030 aluminum and the bottom bar is ASTM A387 grade 2 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 5.6 to 8.0
25
Fatigue Strength, MPa 91 to 110
190 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 220 to 250
300 to 350
Tensile Strength: Ultimate (UTS), MPa 370 to 420
470 to 550
Tensile Strength: Yield (Proof), MPa 240 to 270
260 to 350

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 190
420
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 510
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 130
45
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 99
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
2.6
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.0
1.6
Embodied Energy, MJ/kg 150
20
Embodied Water, L/kg 1140
50

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21 to 26
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 390 to 530
180 to 320
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 33 to 38
16 to 20
Strength to Weight: Bending, points 37 to 40
17 to 19
Thermal Diffusivity, mm2/s 50
12
Thermal Shock Resistance, points 16 to 19
14 to 16

Alloy Composition

Aluminum (Al), % 88.9 to 95.2
0
Bismuth (Bi), % 0 to 0.2
0
Carbon (C), % 0
0.050 to 0.21
Chromium (Cr), % 0 to 0.1
0.5 to 0.8
Copper (Cu), % 3.3 to 4.5
0
Iron (Fe), % 0 to 0.7
97.1 to 98.3
Lead (Pb), % 0.8 to 1.5
0
Magnesium (Mg), % 0.5 to 1.3
0
Manganese (Mn), % 0.2 to 1.0
0.55 to 0.8
Molybdenum (Mo), % 0
0.45 to 0.6
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.8
0.15 to 0.4
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.3
0