7075-T7351 is a high-strength aluminum alloy in the T7351 temper condition, specifically engineered for aerospace structural applications where stress corrosion resistance is paramount. The "7075" designation indicates a zinc-based alloy system, while "T7351" refers to a specific heat treatment process that optimizes the balance between strength and corrosion resistance.
7075-T7351 Mechanical Properties vs. Common Alternatives
| Property | 7075-T7351 | 7075-T6 | 6061-T6 |
|---|---|---|---|
| Tensile Strength | 505-510 MPa (73-78 ksi) | 570-580 MPa (82-84 ksi) | 310 MPa (45 ksi) |
| Yield Strength | 435-440 MPa (63-69 ksi) | 500-510 MPa (72-74 ksi) | 270 MPa (39 ksi) |
| Elongation at Break | 11-13% | 7-8% | 12-17% |
| Brinell Hardness | 140-150 HB | 150-160 HB | 95 HB |
| Stress Corrosion Resistance | Excellent (T7351 temper) | Poor (T6 temper) | Good |
| Typical Price Premium | Baseline | -10% to -15% | -40% to -50% |
The T7351 temper is achieved through a solution heat treatment followed by overaging, which deliberately sacrifices some peak strength (compared to T6) to dramatically improve stress corrosion cracking (SCC) resistance. This trade-off is essential for aerospace applications where component failure due to corrosion could have catastrophic consequences.
For Southeast Asian sellers considering entry into the aerospace forgings market, understanding these technical distinctions is fundamental. Buyers don't just purchase "aluminum"—they purchase certified material with specific temper conditions, mill test reports, and traceability documentation. On Alibaba.com, suppliers who clearly communicate these technical specifications in their product listings attract significantly more qualified inquiries from aerospace buyers.

