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7150
AMS 4307 / AlZn6CuMgZr(A) / 7150 / T61511
| Chemical Properties | % Value |
| Silicon (Si) | 0,00 - 0,15 |
| Chromium (Cr) | 0,10 - 0,22 |
| Manganese (Mn) | 0,00 - 0,20 |
| Magnesium (Mg) | 2,00 - 2,90 |
| Copper (Cu) | 1,2 - 1,90 |
| Titanium (Ti) | 0,00 - 0,10 |
| Iron (Fe) | 0,00 - 0,20 |
| Zinc (Zn) | 7,20 - 8,20 |
| Aluminium (Al) | Balance |
| Titanium + Zirconium (Ti+Zr) | 0,08 - 0,15 |
| Physical Properties | Value |
| Density | 2,86 g/cm³ |
| Thermal Expansion | 24.7 µm/m.°C |
| Modulus of Elasticity | 69,1 GPa |
| Mechanical Properties | Value |
| Proof Strength | min. 537 MPa |
| Yield Strength | min. 580 MPa |
| Shear Strength | min. 490 MPa |
| Elongation A50 mm | 11% |
| Hardness | 160 HB |
| 7150 T61511 Temperature – Ultimate Tensile Strength Graph |
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| 7150 T61511 Thickness – Ultimate Tensile Strength Graph |
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| 7150 T61511 Diameter – Ultimate Tensile Strength Graph |
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| 7150 T61511 Diameter-Yield Tensile Strength |
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7150-T61511 aluminum alloy is a zinc (Zn)-based alloy belonging to the 7xxx series, developed for high-strength applications. The T61511 temper is achieved through a controlled precipitation hardening process combined with stress-relieving operations. This provides both high strength and good dimensional stability. While chemically similar to 7075, 7150 is specifically optimized for performance in thick sections.
In terms of strength, 7150-T61511 offers very high yield and tensile strength, particularly in thick plates and forgings, where it provides more uniform mechanical properties than 7075-T6. Compared to 7050, it delivers similar strength levels but may exhibit better fracture toughness and lower crack propagation tendency, making it suitable for critical structural applications.
Regarding corrosion resistance, 7150 is specifically designed to improve resistance to stress corrosion cracking (SCC). It performs significantly better than 7075-T6 in this regard and is comparable to 7050. Although it does not match the marine corrosion resistance of 5xxx series alloys such as 5083, it provides reliable performance for aerospace environments. Surface protection such as anodizing or coating is commonly applied.
In terms of machinability and formability, 7150-T61511 offers good machinability, though its formability is more limited compared to the O temper. Complex forming operations are typically performed in softer tempers. Compared to 6061, machinability is considered similar, although higher strength can lead to increased tool wear. Weldability is generally poor, similar to other 7xxx alloys, while 6xxx alloys perform better in welding.
Regarding vibration response and applications, 7150-T61511 is widely used in aerospace and defense industries, particularly in wing structures, fuselage components, and heavily loaded structural parts. Its high specific strength, good fatigue resistance, and crack growth resistance make it ideal for long-life applications. While 2024 is used in sheet structures, 7075 in general high-strength applications, and 7050 in thick aerospace sections, 7150 offers an optimized balance among these alloys.
7150 T61511 can be supplied in accordance with the following standards.
• 7150 T61511 Extruded Bar; AMS 4307, UNS A97150, ISO AlZn6CuMgZr, ASTM B221
• 7150 T61511 Extruded Flat Bar; AMS 4307, UNS A97150, ISO AlZn6CuMgZr, ASTM B221
• 7150 T61511 Extruded Tube; AMS 4307, UNS A97150, ISO AlZn6CuMgZr, ASTM B221
Selection Factors for 7150 T61511
- Strength: High
- Machinability: Good
- Weldability: Medium
- Formability: Poor
- Corrosion Resistance: Very good
- Heat Treatment: Yes
Some Known Applications for 7150 T61511
As an aircraft seat rail component,
In engine structures,
Also used in stringers.
7150 T61511 is manufactured and supplied in round/flat bar and tube/profile forms.
- Round/Flat Bar
- Tube/Profile
| Mechanical Properties | |||
| Thickness (mm) | Proof Strength (Min.) | Yield Strength (Min.) | Elongation A50 mm % |
| 25,4 mm | 565 MPa | 607 MPa | %11 |




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