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ASTM A369 Grade FP9 vs. 333.0 Aluminum

ASTM A369 grade FP9 belongs to the iron alloys classification, while 333.0 aluminum belongs to the aluminum 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 ASTM A369 grade FP9 and the bottom bar is 333.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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