Product Introduction:

HWA-CQ-85 is a hybrid oil electric vertical takeoff and landing fixed wing unmanned aerial vehicle, equipped with advanced oil powered engines and powerful power drive. It combines the advantages of electric rotors and adopts a hybrid oil powered driving method. It also has the ability to perform vertical takeoff and landing for quadcopters and fast cruising for fixed wing aircraft, and can adapt to various complex takeoff and landing environments. According to the design of multi payload missions, there is a super large payload compartment under the fuselage, with a maximum effective load of 25 kilograms, truly achieving multi-purpose use of one aircraft for field operations. Can be used for surveying, power line patrol, target drones and other scenarios.

TECHNICAL INDEX

• Takeoff and Landing Method: Vertical Takeoff and Landing

• Power system: hybrid oil electric power

• Wing span/fuselage length: 5m/3.02m

• Maximum takeoff weight: 85kg

• Maximum payload weight: 25kg

• Cruise speed: 120km/h

• Flight time:> 6h (20kg load)

• Maximum altitude: 5000m

• Control radius: 100km (optional)

application area

It can mount various mission payloads such as electro-optical pods and SAR radars to perform different tasks. Mainly used for target drones, customers are distributed in weapon research institutions and military units.