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6070 Aluminum vs. ASTM A387 Grade 21 Steel

6070 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 (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 6070 aluminum and the bottom bar is ASTM A387 grade 21 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 5.6 to 8.6
21
Fatigue Strength, MPa 95 to 130
160 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 220 to 240
310 to 370
Tensile Strength: Ultimate (UTS), MPa 370 to 380
500 to 590
Tensile Strength: Yield (Proof), MPa 350
230 to 350

Thermal Properties

Latent Heat of Fusion, J/g 410
260
Maximum Temperature: Mechanical, °C 160
480
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 570
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 160
41
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 140
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.1
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
1.8
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1170
62

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 20 to 32
84 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 900
140 to 320
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 38
18 to 21
Strength to Weight: Bending, points 42 to 43
18 to 20
Thermal Diffusivity, mm2/s 65
11
Thermal Shock Resistance, points 16 to 17
14 to 17

Alloy Composition

Aluminum (Al), % 94.6 to 98
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0 to 0.1
2.8 to 3.3
Copper (Cu), % 0.15 to 0.4
0
Iron (Fe), % 0 to 0.5
94.4 to 96
Magnesium (Mg), % 0.5 to 1.2
0
Manganese (Mn), % 0.4 to 1.0
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 1.0 to 1.7
0 to 0.5
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