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5086 Aluminum vs. ASTM Grade HT Steel

5086 aluminum belongs to the aluminum alloys classification, while ASTM grade HT steel 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 5086 aluminum and the bottom bar is ASTM grade HT steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 65 to 100
150
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.7 to 20
4.6
Fatigue Strength, MPa 88 to 180
130
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 270 to 390
500
Tensile Strength: Yield (Proof), MPa 110 to 320
270

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Corrosion, °C 65
400
Maximum Temperature: Mechanical, °C 190
1010
Melting Completion (Liquidus), °C 640
1390
Melting Onset (Solidus), °C 590
1340
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 24
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.8
5.4
Embodied Energy, MJ/kg 150
76
Embodied Water, L/kg 1180
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
19
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
180
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 28 to 40
18
Strength to Weight: Bending, points 34 to 44
18
Thermal Diffusivity, mm2/s 52
3.2
Thermal Shock Resistance, points 12 to 17
12

Alloy Composition

Aluminum (Al), % 93 to 96.3
0
Carbon (C), % 0
0.35 to 0.75
Chromium (Cr), % 0.050 to 0.25
15 to 19
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
38.2 to 51.7
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
33 to 37
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.4
0 to 2.5
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0