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333.0 Aluminum vs. ASTM A369 Grade FP9

333.0 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP9 belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 333.0 aluminum and the bottom bar is ASTM A369 grade FP9.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 90 to 110
140
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 1.0 to 2.0
20
Fatigue Strength, MPa 83 to 100
160
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 28
75
Shear Strength, MPa 190 to 230
300
Tensile Strength: Ultimate (UTS), MPa 230 to 280
470
Tensile Strength: Yield (Proof), MPa 130 to 210
240

Thermal Properties

Latent Heat of Fusion, J/g 520
270
Maximum Temperature: Mechanical, °C 170
600
Melting Completion (Liquidus), °C 590
1450
Melting Onset (Solidus), °C 530
1410
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 100 to 140
26
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
9.0
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
10

Otherwise Unclassified Properties

Base Metal Price, % relative 10
6.5
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 7.6
2.0
Embodied Energy, MJ/kg 140
28
Embodied Water, L/kg 1040
87

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
80
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
140
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 22 to 27
17
Strength to Weight: Bending, points 29 to 34
17
Thermal Diffusivity, mm2/s 42 to 57
6.9
Thermal Shock Resistance, points 11 to 13
13

Alloy Composition


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Aluminum (Al), % 81.8 to 89
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
8.0 to 10
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 1.0
87.1 to 90.3
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.5
0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 8.0 to 10
0.5 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0