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5056 Aluminum vs. ASTM A369 Grade FP92

5056 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP92 belongs to the iron 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 5056 aluminum and the bottom bar is ASTM A369 grade FP92.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 4.9 to 31
19
Fatigue Strength, MPa 140 to 200
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
76
Shear Strength, MPa 170 to 240
440
Tensile Strength: Ultimate (UTS), MPa 290 to 460
710
Tensile Strength: Yield (Proof), MPa 150 to 410
490

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 190
590
Melting Completion (Liquidus), °C 640
1490
Melting Onset (Solidus), °C 570
1450
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 130
26
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
9.3
Electrical Conductivity: Equal Weight (Specific), % IACS 99
10

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 9.0
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1180
89

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 140
120
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 1220
620
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 30 to 48
25
Strength to Weight: Bending, points 36 to 50
22
Thermal Diffusivity, mm2/s 53
6.9
Thermal Shock Resistance, points 13 to 20
19

Alloy Composition

Aluminum (Al), % 93 to 95.4
0 to 0.020
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0.050 to 0.2
8.5 to 9.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
85.8 to 89.1
Magnesium (Mg), % 4.5 to 5.6
0
Manganese (Mn), % 0.050 to 0.2
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 0.3
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
0.15 to 0.25
Zinc (Zn), % 0 to 0.1
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.15
0