S-80 Large Double Tailed Fixed Wing Unmanned Target Aircraft System

▲The aircraft is a conventional layout, composite fixed wing drone. It adopts the commonly used dual tail brace design layout of
military drones, with a rear push power system. The wing design adopts a high lift airfoil typical of military drones with a high lift to drag
ratio and excellent flight performance. The wingtip design has winglets, greatly reducing wingtip induced drag and achieving excellent
flight performance. In addition, the fuselage design has increased the cabin to provide greater equipment installation space for the
mission payload, with a maximum load capacity of 20kg, making it very suitable for mounting specialized mission equipment such as
target spot detectors, corner reflectors, and miniSAR. Mission equipment can also be installed below the wing after modification.
▲ The system has high reliability and convenient maneuverability, adopting the methods of taxiing takeoff and taxiing landing. By
installing autonomous takeoff and landing assistance equipment, it can have fully autonomous flight characteristics, providing users
with more convenient and reliable control, more flexible application, and simplified training requirements for operators. The drone can
fill up to 40 liters of fuel and has a relatively long range among drones of the same class. In addition, the fuselage can be equipped with
a recovery umbrella, which can be opened and landed in emergency situations, ensuring the safety of the aircraft and ground facilities.
▲ The power is an oil powered internal combustion engine, with sufficient driving time, stable and reliable operation, and convenient
use.
▲ The fuselage can carry a retrieval umbrella, which can be opened and landed in emergency situations, ensuring the safety of the
aircraft and ground facilities