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ASTM A369 Grade FP22 vs. 1100A Aluminum

ASTM A369 grade FP22 belongs to the iron alloys classification, while 1100A aluminum belongs to the aluminum alloys. There are 30 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 FP22 and the bottom bar is 1100A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 20
4.5 to 34
Fatigue Strength, MPa 160
35 to 74
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 300
59 to 99
Tensile Strength: Ultimate (UTS), MPa 470
89 to 170
Tensile Strength: Yield (Proof), MPa 240
29 to 150

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 460
170
Melting Completion (Liquidus), °C 1470
640
Melting Onset (Solidus), °C 1430
640
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 39
230
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
60
Electrical Conductivity: Equal Weight (Specific), % IACS 8.7
200

Otherwise Unclassified Properties

Base Metal Price, % relative 3.8
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 1.7
8.2
Embodied Energy, MJ/kg 23
150
Embodied Water, L/kg 58
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 80
6.4 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 150
5.9 to 150
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 17
9.1 to 17
Strength to Weight: Bending, points 17
16 to 25
Thermal Diffusivity, mm2/s 11
93
Thermal Shock Resistance, points 14
4.0 to 7.6

Alloy Composition

Aluminum (Al), % 0
99 to 100
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 1.9 to 2.6
0
Copper (Cu), % 0
0.050 to 0.2
Iron (Fe), % 95 to 96.9
0 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0.3 to 0.6
0 to 0.050
Molybdenum (Mo), % 0.87 to 1.1
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 1.0
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15