S24 Vertical Takeoff and Landing Fixed Wing Unmanned Aerial Vehicle

▲Advanced design

The aircraft adopts the internationally commonly used double tail strut fixed wing aerodynamic layout and adopts a high-performance gliding wing shape, which has a high glide ratio and excellent gliding performance. It can achieve long endurance and long-distance operation flight. The tail strut four rotor design can achieve vertical takeoff and landing on small fields. The body material is carbon fiber, with light weight and high strength. Fiberglass Kevlar material can also be used, with lower RCS, suitable for long-term reconnaissance operations.

▲ Strong load capacity

With a maximum load of 6KG, it can be mounted in a dual light pod for long-distance reconnaissance missions, meeting various mission environments;

▲ Powerful engine

The power adopts a four stroke internal combustion engine, with low fuel consumption, quiet sound, and low vibration; Adopting high-efficiency carbon fiber propellers, the power is stable and reliable, suitable for long-term flight;