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ASTM A369 Grade FP92 vs. 5059 Aluminum

ASTM A369 grade FP92 belongs to the iron alloys classification, while 5059 aluminum belongs to the aluminum alloys. There are 30 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 FP92 and the bottom bar is 5059 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 19
11 to 25
Fatigue Strength, MPa 330
170 to 240
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 440
220 to 250
Tensile Strength: Ultimate (UTS), MPa 710
350 to 410
Tensile Strength: Yield (Proof), MPa 490
170 to 300

Thermal Properties

Latent Heat of Fusion, J/g 260
390
Maximum Temperature: Mechanical, °C 590
210
Melting Completion (Liquidus), °C 1490
650
Melting Onset (Solidus), °C 1450
510
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 26
110
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
29
Electrical Conductivity: Equal Weight (Specific), % IACS 10
95

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 2.8
9.1
Embodied Energy, MJ/kg 40
160
Embodied Water, L/kg 89
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
42 to 75
Resilience: Unit (Modulus of Resilience), kJ/m3 620
220 to 650
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25
36 to 42
Strength to Weight: Bending, points 22
41 to 45
Thermal Diffusivity, mm2/s 6.9
44
Thermal Shock Resistance, points 19
16 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.020
89.9 to 94
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0 to 0.25
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 85.8 to 89.1
0 to 0.5
Magnesium (Mg), % 0
5.0 to 6.0
Manganese (Mn), % 0.3 to 0.6
0.6 to 1.2
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
0 to 0.45
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
0.4 to 0.9
Zirconium (Zr), % 0 to 0.010
0.050 to 0.25
Residuals, % 0
0 to 0.15