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VF13E Chinese Unmanned Aerial Vehicle (UAV)

VF13E

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
VF13E Chinese Unmanned Aerial Vehicle (UAV)
Designation
VF13E
Alternate Designation
VF13E
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Hinaray
Date of Introduction
2021
Description

The VF13E Chinese Unmanned Aerial Vehicle (UAV) is a hybrid electric vertical takeoff and landing (VTOL) fixed-wing platform developed by Hinaray. Designed for both commercial and tactical applications, the VF13E integrates multirotor hovering with fixed-wing cruise efficiency to provide extended endurance, modular payload options, and rapid deployment. These features make it suitable for surveillance, infrastructure inspection, mapping, and defense reconnaissance. The compact design, three-minute assembly process, and integration-ready architecture enable operational flexibility for organizations that require hybrid aerial capabilities without requiring runway infrastructure. As an electric hybrid VTOL platform, the VF13E differentiates itself from conventional fixed-wing UAVs by incorporating vertical lift systems that support autonomous takeoff and landing in challenging environments. In contrast to multirotor-only systems, which rely solely on rotary lift, the VF13E uses four vertical lift motors for VTOL operations and a single rear pusher propeller for fixed-wing flight. An advanced flight control system manages transitions between these modes. This hybrid approach addresses a key operational limitation: traditional fixed-wing aircraft require runways or catapults, whereas multirotor systems typically have limited endurance, with flight times of 30 to 90 minutes. The VF13E supports a swappable payload system compatible with a range of specialized aerial imaging and sensing equipment. ​ Electro-optical systems: Digital single-lens reflex (DSLR) and compact cameras designed for high-resolution reconnaissance photography. Advanced sensors: LiDAR units for topographic mapping and structural analysis. Multispectral imaging: Payloads designed for agricultural assessment and environmental monitoring. Thermal reconnaissance: Infrared cameras for night-time or concealed-target identification. Custom payloads: Modular integration supports a variety of mission-specific sensors within a two-kilogram payload capacity.

Air & Air Defense Specifications
Engine Electric (22 hp)
Max Speed 100.0 km/h
Cruise Speed 100.0 km/h
Range 150.0 km
Endurance 210.00 hrs
Service Ceiling 1500 m
Wingspan 2.50 m
Payload Capacity 2 kg
System
Alternate Designation VF13E
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Hinaray
Payload Capacity 2.0 kg
Mission Planning and Execution Operators define departure/arrival waypoints and sensor acquisition parameters through GCS interface; the flight controller manages automatic vertical ascent to cruise altitude, fixed-wing transition, autonomous sensor payload management, and controlled descent with vertical landing. Redundant flight controller architecture provides fault tolerance for loss-of-signal contingencies, automatically executing RTL procedures upon communication interruption. Ground control range extends from one-kilometer direct line-of-sight (LOS) manual operation to 30+ kilometer beyond-line-of-sight (BLOS) autonomous mission execution, dependent upon communication link fidelity and regulatory airspace authorization.
Noise Level Below 65 dB
Ingress Protection IP54
Dimensions
Length 1.62 m
Height INA
Wingspan 2.5 m
Maximum Takeoff Weight 13.5 kg
Automotive
Engine Name 2 x T-MOTOR AT4130 KV230
Engine Type Brushless motor
Engine Power 22 kg combined thrust
Battery Battery management employs lithium polymer chemistry with 12-series high-voltage configuration, enabling extended cruise phases through efficient aerodynamic lift generation. The hybrid architecture differentiates endurance performance: with one-kilogram payload, the VF13E achieves 210 minutes endurance; payload degradation curves suggest approximately 60-90 minute missions with maximum two-kilogram payloads. This endurance profile positions the platform between short-duration multirotor systems (45-90 minutes) and extreme-endurance fuel-powered alternatives (180-360+ minutes), establishing it as optimal for single-sortie operational missions not requiring extreme persistence.
Maximum Speed INA
Cruise Speed 100 km/h
Maximum Range 150 km
Service Ceiling 1,500 m
Endurance 210 minutes (with 1kg payload)
Wind Resistance Grade 6 conditions (12 m/s)
Details
Country of Origin China
Category UAVs
Air > UAVs
Filter Label
V
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
1.62 m
Width
2.5 m
Height
Weight
13.5 kg
Operators (1)
China
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