The remote unmanned reconnaissance aircraft system adopts a dual tail strut aerodynamic design, which greatly reduces the overall size of the aircraft platform while increasing its maneuverability. After disassembling the aircraft platform, it can be transported and stored in a very small space. The mission payload system can be adjusted according to actual combat needs, including optoelectronic pods, SAR, optical array sensors, small air to ground missiles, etc.

Takeoff and landing wind speed:<10.8m/s
Practical ceiling: 7000M
Wing span: 9.3M
Takeoff methods: wheeled, catapult, vehicle mounted, rocket assisted
Control radius: 200KM (for wireless TV)>1000KM (for satellite TV)
Body height: 1.5M
Maximum takeoff weight: 370KG
Recycling methods: wheeled, parachute
Body length: 5.6M
Engine: Aviation piston engine
Task payload: 70KG
Cruise speed: 140-180km/h
Flight time:>10h
Maximum speed: 200KM/h