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6005 Aluminum vs. ASTM A182 Grade F3V

6005 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F3V belongs to the iron alloys. There are 31 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 6005 aluminum and the bottom bar is ASTM A182 grade F3V.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 90 to 95
210
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 9.5 to 17
20
Fatigue Strength, MPa 55 to 95
330
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 120 to 210
410
Tensile Strength: Ultimate (UTS), MPa 190 to 310
660
Tensile Strength: Yield (Proof), MPa 100 to 280
470

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 160
470
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 610
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 180 to 200
39
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 180
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.2
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
2.3
Embodied Energy, MJ/kg 150
33
Embodied Water, L/kg 1180
63

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 36
120
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 550
590
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 20 to 32
23
Strength to Weight: Bending, points 28 to 38
21
Thermal Diffusivity, mm2/s 74 to 83
10
Thermal Shock Resistance, points 8.6 to 14
19

Alloy Composition

Aluminum (Al), % 97.5 to 99
0
Boron (B), % 0
0.0010 to 0.0030
Carbon (C), % 0
0.050 to 0.18
Chromium (Cr), % 0 to 0.1
2.8 to 3.2
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.35
94.4 to 95.7
Magnesium (Mg), % 0.4 to 0.6
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 0.020
Silicon (Si), % 0.6 to 0.9
0 to 0.1
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.1
0.015 to 0.035
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0