When engineers specify ultra-high strength aluminum for critical applications, 7075 has long been the default choice. However, a newer alloy—7068—is quietly reshaping expectations for what aluminum can achieve. With yield strength reaching 700MPa, 7068 delivers 15-20% higher strength than 7075 while maintaining comparable corrosion resistance and better high-temperature performance [1].
For B2B buyers sourcing materials on Alibaba.com, understanding the technical distinctions between these alloys is essential. The wrong material selection can lead to premature failure, certification issues, or unnecessary cost premiums. This guide provides the technical foundation you need to make informed decisions when selling on Alibaba.com or procuring from global suppliers.
7068 vs 7075 Aluminum: Head-to-Head Technical Comparison
| Property | 7068-T6 | 7075-T6 | Advantage |
|---|---|---|---|
| Ultimate Tensile Strength | 710 MPa | 572 MPa | 7068 +24% |
| Yield Strength | 690 MPa | 503 MPa | 7068 +37% |
| Elongation at Break | 8-10% | 11% | 7075 +10% |
| Density | 2.81 g/cm³ | 2.81 g/cm³ | Equal |
| Hardness (Brinell) | 185 HB | 150 HB | 7068 +23% |
| Primary Alloying Element | Zinc 7.3-8.3% | Zinc 5.1-6.1% | 7068 higher Zn |
| Cost Premium | 30-50% higher | Baseline | 7075 more economical |
| Availability | Limited suppliers | Widely available | 7075 easier to source |
The chemistry tells the story: 7068 contains higher zinc content (7.3-8.3% vs 5.1-6.1%) along with magnesium (2.2-3.0%) and copper (1.6-2.4%), plus trace zirconium (0.05-0.15%) for grain refinement [5]. This optimized composition enables the exceptional strength characteristics that have earned 7068 FAA and NASA certification for aerospace applications [1].

