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850.0 Aluminum vs. ASTM A387 Grade 2 Steel

850.0 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 2 steel belongs to the iron alloys. There are 31 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 850.0 aluminum and the bottom bar is ASTM A387 grade 2 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 45
140 to 170
Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 7.9
25
Fatigue Strength, MPa 59
190 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 100
300 to 350
Tensile Strength: Ultimate (UTS), MPa 140
470 to 550
Tensile Strength: Yield (Proof), MPa 76
260 to 350

Thermal Properties

Latent Heat of Fusion, J/g 380
250
Maximum Temperature: Mechanical, °C 190
420
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 370
1420
Specific Heat Capacity, J/kg-K 850
470
Thermal Conductivity, W/m-K 180
45
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 47
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 140
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 14
2.6
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.5
1.6
Embodied Energy, MJ/kg 160
20
Embodied Water, L/kg 1160
50

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.1
98 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 42
180 to 320
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 44
24
Strength to Weight: Axial, points 12
16 to 20
Strength to Weight: Bending, points 19
17 to 19
Thermal Diffusivity, mm2/s 69
12
Thermal Shock Resistance, points 6.1
14 to 16

Alloy Composition


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Aluminum (Al), % 88.3 to 93.1
0
Carbon (C), % 0
0.050 to 0.21
Chromium (Cr), % 0
0.5 to 0.8
Copper (Cu), % 0.7 to 1.3
0
Iron (Fe), % 0 to 0.7
97.1 to 98.3
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.1
0.55 to 0.8
Molybdenum (Mo), % 0
0.45 to 0.6
Nickel (Ni), % 0.7 to 1.3
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.7
0.15 to 0.4
Sulfur (S), % 0
0 to 0.025
Tin (Sn), % 5.5 to 7.0
0
Titanium (Ti), % 0 to 0.2
0
Residuals, % 0 to 0.3
0