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6061 Aluminum vs. ASTM A387 Grade 2 Steel

6061 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 (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 6061 aluminum and the bottom bar is ASTM A387 grade 2 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 3.4 to 20
25
Fatigue Strength, MPa 58 to 110
190 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 84 to 210
300 to 350
Tensile Strength: Ultimate (UTS), MPa 130 to 410
470 to 550
Tensile Strength: Yield (Proof), MPa 76 to 370
260 to 350

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 170
420
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 580
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 170
45
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 43
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 140
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.6
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
1.6
Embodied Energy, MJ/kg 150
20
Embodied Water, L/kg 1180
50

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.8 to 81
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 42 to 1000
180 to 320
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 13 to 42
16 to 20
Strength to Weight: Bending, points 21 to 45
17 to 19
Thermal Diffusivity, mm2/s 68
12
Thermal Shock Resistance, points 5.7 to 18
14 to 16

Alloy Composition

Aluminum (Al), % 95.9 to 98.6
0
Carbon (C), % 0
0.050 to 0.21
Chromium (Cr), % 0.040 to 0.35
0.5 to 0.8
Copper (Cu), % 0.15 to 0.4
0
Iron (Fe), % 0 to 0.7
97.1 to 98.3
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0 to 0.15
0.55 to 0.8
Molybdenum (Mo), % 0
0.45 to 0.6
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0.4 to 0.8
0.15 to 0.4
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants