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5657 Aluminum vs. ASTM A369 Grade FP92

5657 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP92 belongs to the iron 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 5657 aluminum and the bottom bar is ASTM A369 grade FP92.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 50
210
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.6 to 15
19
Fatigue Strength, MPa 74 to 88
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 92 to 110
440
Tensile Strength: Ultimate (UTS), MPa 150 to 200
710
Tensile Strength: Yield (Proof), MPa 140 to 170
490

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 180
590
Melting Completion (Liquidus), °C 660
1490
Melting Onset (Solidus), °C 640
1450
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 210
26
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
9.3
Electrical Conductivity: Equal Weight (Specific), % IACS 180
10

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.4
2.8
Embodied Energy, MJ/kg 160
40
Embodied Water, L/kg 1200
89

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.7 to 27
120
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 200
620
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 15 to 20
25
Strength to Weight: Bending, points 23 to 28
22
Thermal Diffusivity, mm2/s 84
6.9
Thermal Shock Resistance, points 6.7 to 8.6
19

Alloy Composition


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Aluminum (Al), % 98.5 to 99.4
0 to 0.020
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0
8.5 to 9.5
Copper (Cu), % 0 to 0.1
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.1
85.8 to 89.1
Magnesium (Mg), % 0.6 to 1.0
0
Manganese (Mn), % 0 to 0.030
0.3 to 0.6
Molybdenum (Mo), % 0
0.3 to 0.6
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.040 to 0.090
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.080
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0 to 0.010
Tungsten (W), % 0
1.5 to 2.0
Vanadium (V), % 0 to 0.050
0.15 to 0.25
Zinc (Zn), % 0 to 0.050
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.050
0