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7050 Aluminum vs. ASTM A369 Grade FP91

7050 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP91 belongs to the iron 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 7050 aluminum and the bottom bar is ASTM A369 grade FP91.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2 to 12
19
Fatigue Strength, MPa 130 to 210
320
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
75
Shear Strength, MPa 280 to 330
410
Tensile Strength: Ultimate (UTS), MPa 490 to 570
670
Tensile Strength: Yield (Proof), MPa 390 to 500
460

Thermal Properties

Latent Heat of Fusion, J/g 370
270
Maximum Temperature: Mechanical, °C 190
600
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 490
1420
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 140
26
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
8.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
10

Otherwise Unclassified Properties

Base Metal Price, % relative 10
7.0
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.6
Embodied Energy, MJ/kg 150
37
Embodied Water, L/kg 1120
88

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
110
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
560
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
24
Strength to Weight: Bending, points 45 to 50
22
Thermal Diffusivity, mm2/s 54
6.9
Thermal Shock Resistance, points 21 to 25
18

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0 to 0.020
Carbon (C), % 0
0.080 to 0.12
Chromium (Cr), % 0 to 0.040
8.0 to 9.5
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
87.3 to 90.3
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0.3 to 0.6
Molybdenum (Mo), % 0
0.85 to 1.1
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.060 to 0.1
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.12
0.2 to 0.5
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.060
0 to 0.010
Vanadium (V), % 0
0.18 to 0.25
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0 to 0.010
Residuals, % 0 to 0.15
0