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ASTM A369 Grade FP92 vs. 771.0 Aluminum

ASTM A369 grade FP92 belongs to the iron alloys classification, while 771.0 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 771.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
85 to 120
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 19
1.7 to 6.5
Fatigue Strength, MPa 330
92 to 180
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 76
26
Tensile Strength: Ultimate (UTS), MPa 710
250 to 370
Tensile Strength: Yield (Proof), MPa 490
210 to 350

Thermal Properties

Latent Heat of Fusion, J/g 260
380
Maximum Temperature: Mechanical, °C 590
180
Melting Completion (Liquidus), °C 1490
630
Melting Onset (Solidus), °C 1450
620
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 26
140 to 150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
27
Electrical Conductivity: Equal Weight (Specific), % IACS 10
82

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 2.8
8.0
Embodied Energy, MJ/kg 40
150
Embodied Water, L/kg 89
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
4.4 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 620
310 to 900
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
46
Strength to Weight: Axial, points 25
23 to 35
Strength to Weight: Bending, points 22
29 to 39
Thermal Diffusivity, mm2/s 6.9
54 to 58
Thermal Shock Resistance, points 19
11 to 16

Alloy Composition


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Aluminum (Al), % 0 to 0.020
90.5 to 92.5
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0.060 to 0.2
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 85.8 to 89.1
0 to 0.15
Magnesium (Mg), % 0
0.8 to 1.0
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
0 to 0.15
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0.1 to 0.2
Tungsten (W), % 1.5 to 2.0
0
Vanadium (V), % 0.15 to 0.25
0
Zinc (Zn), % 0
6.5 to 7.5
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15