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ASTM A369 Grade FP92 vs. 1350 Aluminum

ASTM A369 grade FP92 belongs to the iron alloys classification, while 1350 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 1350 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
20 to 45
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 19
1.4 to 30
Fatigue Strength, MPa 330
24 to 50
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 440
44 to 110
Tensile Strength: Ultimate (UTS), MPa 710
68 to 190
Tensile Strength: Yield (Proof), MPa 490
25 to 170

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 590
170
Melting Completion (Liquidus), °C 1490
660
Melting Onset (Solidus), °C 1450
650
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 26
230
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
61 to 62
Electrical Conductivity: Equal Weight (Specific), % IACS 10
200 to 210

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
8.3
Embodied Energy, MJ/kg 40
160
Embodied Water, L/kg 89
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
0.77 to 54
Resilience: Unit (Modulus of Resilience), kJ/m3 620
4.4 to 200
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25
7.0 to 19
Strength to Weight: Bending, points 22
14 to 27
Thermal Diffusivity, mm2/s 6.9
96
Thermal Shock Resistance, points 19
3.0 to 8.2

Alloy Composition

Aluminum (Al), % 0 to 0.020
99.5 to 100
Boron (B), % 0.0010 to 0.0060
0 to 0.050
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0 to 0.010
Copper (Cu), % 0
0 to 0.050
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 85.8 to 89.1
0 to 0.4
Manganese (Mn), % 0.3 to 0.6
0 to 0.010
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 0.1
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.020
Tungsten (W), % 1.5 to 2.0
0
Vanadium (V), % 0.15 to 0.25
0 to 0.020
Zinc (Zn), % 0
0 to 0.050
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.1