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VF-200P Chinese Unmanned Aerial Vehicle (UAV)

VF-200P

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
VF-200P Chinese Unmanned Aerial Vehicle (UAV)
Designation
VF-200P
Alternate Designation
VF-200P
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Hinaray
Date of Introduction
2025
Description

The VF-200P Chinese Unmanned Aerial Vehicle (UAV) is a heavy-lift, long-endurance Hybrid VTOL (Vertical Take-Off and Landing) Fixed-Wing UAV manufactured by Chinese defense and aerospace entity Hinaray (also associated with Shenzhen SkyWing UAV Technology Co., Ltd.). As of late 2025, the platform is marketed as a "dual-use" system, primarily optimized for logistics, emergency response, and heavy-payload surveillance. While distinct from dedicated strike platforms like the Wing Loong series, its high payload capacity and autonomous capabilities make it a viable asset for military logistics and intelligence support. The VF-200P utilizes a composite aerodynamic layout, featuring a fixed wing for efficient cruising and quad-rotors for vertical lift. This configuration allows it to operate from improved or unimproved sites without a runway, a critical capability for forward-deployed military logistics or disaster relief in austere environments. Features dual RTK GNSS (Real-Time Kinematic Global Navigation Satellite System) for centimeter-level positioning accuracy, essential for autonomous landing and precise cargo drops. The system's modular design allows it to be rapidly reconfigured from a cargo carrier to a sensor platform, aligning with the PLA's broader push for "civil-military fusion" where platforms can serve both commercial and defense needs seamlessly.

Air & Air Defense Specifications
Engine The aircraft uses a hybrid power system. A 342cc EFI (Electronic Fuel Injection) engine powers the rear pusher propeller for efficient, long-endurance cruising, while electric motors power the four vertical lift rotors for takeoff and landing. This "oil-activated" hybrid approach allows it to achieve flight times significantly longer than pure electric VTOLs.
Max Speed 120.0 km/h
Cruise Speed 80.0 km/h
Range 400.0 km
Endurance 4.00 hrs
Service Ceiling 5000 m
Wingspan 6.66 m
Payload Capacity 60 kg
System
Alternate Designation VF-200P
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Hinaray
Construction Airframe built from carbon fiber composites for high strength-to-weight ratio.
Payload Capacity 60 kg
Autonomy Includes autonomous return-to-home functionality in case of datalink loss.
Dimensions
Length 3.85 m
Height INA
Wingspan 6.66 m
Maximum Takeoff Weight 200 kg
Automotive
Engine Name INA
Engine Type The aircraft uses a hybrid power system. A 342cc EFI (Electronic Fuel Injection) engine powers the rear pusher propeller for efficient, long-endurance cruising, while electric motors power the four vertical lift rotors for takeoff and landing. This "oil-activated" hybrid approach allows it to achieve flight times significantly longer than pure electric VTOLs.
Engine Power INA
Maximum Speed 120 km/h
Cruise Speed 80 km/h
Maximum Range 400 km
Service Ceiling 5,000 m
Endurance 4 hours (at 50 kg payload)
Wind Resistance Rated for Level 6 winds (12 m/s), allowing operation in adverse weather conditions.
Details
Country of Origin China
Category UAVs
Air > UAVs
Filter Label
V
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
3.85 m
Width
6.66 m
Height
Weight
200 kg
Operators (1)
China
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