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7050 Aluminum vs. ASTM A369 Grade FP92

7050 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 (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 FP92.

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
330
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 280 to 330
440
Tensile Strength: Ultimate (UTS), MPa 490 to 570
710
Tensile Strength: Yield (Proof), MPa 390 to 500
490

Thermal Properties

Latent Heat of Fusion, J/g 370
260
Maximum Temperature: Mechanical, °C 190
590
Melting Completion (Liquidus), °C 630
1490
Melting Onset (Solidus), °C 490
1450
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
9.3
Electrical Conductivity: Equal Weight (Specific), % IACS 100
10

Otherwise Unclassified Properties

Base Metal Price, % relative 10
11
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.2
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1120
89

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
120
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
620
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 45 to 51
25
Strength to Weight: Bending, points 45 to 50
22
Thermal Diffusivity, mm2/s 54
6.9
Thermal Shock Resistance, points 21 to 25
19

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0 to 0.020
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0 to 0.040
8.5 to 9.5
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
85.8 to 89.1
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
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 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.060
0 to 0.010
Tungsten (W), % 0
1.5 to 2.0
Vanadium (V), % 0
0.15 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