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ASTM A369 Grade FP11 vs. 206.0 Aluminum

ASTM A369 grade FP11 belongs to the iron alloys classification, while 206.0 aluminum belongs to the aluminum 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 ASTM A369 grade FP11 and the bottom bar is 206.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140
95 to 110
Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 20
8.4 to 12
Fatigue Strength, MPa 160
88 to 210
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
27
Shear Strength, MPa 300
260
Tensile Strength: Ultimate (UTS), MPa 470
330 to 440
Tensile Strength: Yield (Proof), MPa 240
190 to 350

Thermal Properties

Latent Heat of Fusion, J/g 260
390
Maximum Temperature: Mechanical, °C 430
170
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1420
570
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 40
120
Thermal Expansion, µm/m-K 13
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.4
33
Electrical Conductivity: Equal Weight (Specific), % IACS 8.5
99

Otherwise Unclassified Properties

Base Metal Price, % relative 2.9
11
Density, g/cm3 7.8
3.0
Embodied Carbon, kg CO2/kg material 1.6
8.0
Embodied Energy, MJ/kg 21
150
Embodied Water, L/kg 52
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 80
24 to 49
Resilience: Unit (Modulus of Resilience), kJ/m3 150
270 to 840
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
46
Strength to Weight: Axial, points 17
30 to 40
Strength to Weight: Bending, points 17
35 to 42
Thermal Diffusivity, mm2/s 11
46
Thermal Shock Resistance, points 14
17 to 23

Alloy Composition

Aluminum (Al), % 0
93.3 to 95.3
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 1.0 to 1.5
0
Copper (Cu), % 0
4.2 to 5.0
Iron (Fe), % 96.1 to 97.7
0 to 0.15
Magnesium (Mg), % 0
0.15 to 0.35
Manganese (Mn), % 0.3 to 0.6
0.2 to 0.5
Molybdenum (Mo), % 0.44 to 0.65
0
Nickel (Ni), % 0
0 to 0.050
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.5 to 1.0
0 to 0.1
Sulfur (S), % 0 to 0.025
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0
0.15 to 0.3
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15