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ASTM A369 Grade FP92 vs. 359.0 Aluminum

ASTM A369 grade FP92 belongs to the iron alloys classification, while 359.0 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 FP92 and the bottom bar is 359.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
90 to 100
Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 19
3.8 to 4.9
Fatigue Strength, MPa 330
100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 440
220 to 230
Tensile Strength: Ultimate (UTS), MPa 710
340 to 350
Tensile Strength: Yield (Proof), MPa 490
250 to 280

Thermal Properties

Latent Heat of Fusion, J/g 260
530
Maximum Temperature: Mechanical, °C 590
170
Melting Completion (Liquidus), °C 1490
600
Melting Onset (Solidus), °C 1450
570
Specific Heat Capacity, J/kg-K 470
910
Thermal Conductivity, W/m-K 26
140
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 10
120

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 7.9
2.6
Embodied Carbon, kg CO2/kg material 2.8
8.0
Embodied Energy, MJ/kg 40
150
Embodied Water, L/kg 89
1090

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
12 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 620
450 to 540
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 24
54
Strength to Weight: Axial, points 25
37 to 38
Strength to Weight: Bending, points 22
42 to 43
Thermal Diffusivity, mm2/s 6.9
59
Thermal Shock Resistance, points 19
16 to 17

Alloy Composition


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Aluminum (Al), % 0 to 0.020
88.9 to 91
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 85.8 to 89.1
0 to 0.2
Magnesium (Mg), % 0
0.5 to 0.7
Manganese (Mn), % 0.3 to 0.6
0 to 0.1
Molybdenum (Mo), % 0.3 to 0.6
0
Nickel (Ni), % 0 to 0.4
0
Niobium (Nb), % 0.040 to 0.090
0
Nitrogen (N), % 0.030 to 0.070
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
8.5 to 9.5
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.2
Tungsten (W), % 1.5 to 2.0
0
Vanadium (V), % 0.15 to 0.25
0
Zinc (Zn), % 0
0 to 0.1
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15