7050-T73510 Aluminum
7050-T73510 aluminum is 7050 aluminum in the T73510 temper. To achieve this temper, the metal is solution heat-treated, stress relieved, then stabilized by artificial overaging. The stress relief is accomplished by stretching the metal by an amount that depends on the type of standard wrought product being made (extrusion or tube). The degree of overaging is chosen so as to maximize stress corrosion resistance. The metal is not straightened after the stretching operation. This temper is closely related to T73511, which permits such straightening.
The graph bars on the material properties cards below compare 7050-T73510 aluminum to: 7000-series alloys (top), all aluminum alloys (middle), and the entire database (bottom). A full bar means this is the highest value in the relevant set. A half-full bar means it's 50% of the highest, and so on.
Mechanical Properties
Elastic (Young's, Tensile) Modulus
70 GPa 10 x 106 psi
Elongation at Break
12 %
Fatigue Strength
190 MPa 27 x 103 psi
Poisson's Ratio
0.32
Shear Modulus
26 GPa 3.8 x 106 psi
Shear Strength
300 MPa 43 x 103 psi
Tensile Strength: Ultimate (UTS)
500 MPa 72 x 103 psi
Tensile Strength: Yield (Proof)
440 MPa 63 x 103 psi
Thermal Properties
Latent Heat of Fusion
370 J/g
Maximum Temperature: Mechanical
190 °C 380 °F
Melting Completion (Liquidus)
630 °C 1170 °F
Melting Onset (Solidus)
490 °C 910 °F
Specific Heat Capacity
860 J/kg-K 0.21 BTU/lb-°F
Thermal Conductivity
140 W/m-K 82 BTU/h-ft-°F
Thermal Expansion
24 µm/m-K
Electrical Properties
Electrical Conductivity: Equal Volume
35 % IACS
Electrical Conductivity: Equal Weight (Specific)
100 % IACS
Otherwise Unclassified Properties
Base Metal Price
10 % relative
Density
3.1 g/cm3 190 lb/ft3
Embodied Carbon
8.2 kg CO2/kg material
Embodied Energy
150 MJ/kg 63 x 103 BTU/lb
Embodied Water
1120 L/kg 130 gal/lb
Common Calculations
Resilience: Ultimate (Unit Rupture Work)
55 MJ/m3
Resilience: Unit (Modulus of Resilience)
1350 kJ/m3
Stiffness to Weight: Axial
13 points
Stiffness to Weight: Bending
45 points
Strength to Weight: Axial
45 points
Strength to Weight: Bending
45 points
Thermal Diffusivity
54 mm2/s
Thermal Shock Resistance
21 points
Alloy Composition
| Al | 87.3 to 92.1 | |
| Zn | 5.7 to 6.7 | |
| Cu | 2.0 to 2.6 | |
| Mg | 1.9 to 2.6 | |
| Zr | 0.080 to 0.15 | |
| Fe | 0 to 0.15 | |
| Si | 0 to 0.12 | |
| Mn | 0 to 0.1 | |
| Ti | 0 to 0.060 | |
| Cr | 0 to 0.040 | |
| res. | 0 to 0.15 |
All values are % weight. Ranges represent what is permitted under applicable standards.
Followup Questions
Further Reading
Aluminum Standards and Data, Aluminum Association Inc., 2013
EN 573-3: Aluminium and aluminium alloys. Chemical composition and form of wrought products. Chemical composition and form of products
Properties and Selection: Nonferrous Alloys and Special-Purpose Materials, ASM Handbook vol. 2, ASM International, 1993