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VF15E Chinese Unmanned Aerial Vehicle (UAV)

VF15E

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
VF15E Chinese Unmanned Aerial Vehicle (UAV)
Designation
VF15E
Alternate Designation
VF15E
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Hinaray and Shenyang Linghang Aviation Science & Technology (LHTechUAV)
Date of Introduction
2021
Description

The VF15E Chinese Unmanned Aerial Vehicle (UAV) is a hybrid Vertical Takeoff and Landing (VTOL) fixed-wing UAV produced by Hinaray Technology Co., Ltd., an aerospace company based in Shenzhen, China. This mid-weight electric reconnaissance and surveillance UAV is designed to bridge the operational gap between small tactical drones and larger, fuel-powered systems. Its primary distinguishing feature is a quad-plane VTOL configuration that eliminates the need for runways while preserving fixed-wing cruise efficiency. This configuration allows deployment from confined areas, which is essential for expeditionary operations, mountainous regions, and urban environments where traditional fixed-wing launch systems are not feasible. The VF15E embodies the hybrid VTOL design philosophy by integrating multirotor hover capabilities with the aerodynamic efficiency of fixed wings. This design addresses three primary operational challenges encountered by small UAV operators: ​ Launch and Recovery Constraints: Traditional fixed-wing UAVs require catapult launch systems, bungee launchers, or runway infrastructure, which are impractical for mobile or austere operational environments. Endurance Limitations: Pure multirotor platforms are limited by short flight durations, typically 20 to 40 minutes, as a result of continuous high-power hovering. Payload Integration: Small UAV platforms must maximize usable payload capacity while maintaining structural integrity. The VF15E addresses these constraints through transitional flight, in which vertical motors enable liftoff and landing, after which the platform transitions to forward flight using aerodynamic lift and deactivates the vertical motors to conserve battery power.

Air & Air Defense Specifications
Engine The T-MOTOR AT4130 KV230 represents a high-efficiency brushless motor optimized for VTOL applications. (230 hp)
Max Speed 110.0 km/h
Cruise Speed 75.0 km/h
Range 250.0 km
Endurance 210.00 hrs
Service Ceiling 4000 m
Wingspan 2.60 m
Payload Capacity 1 kg
System
Alternate Designation VF15E
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Hinaray and Shenyang Linghang Aviation Science & Technology (LHTechUAV)
Payload Capacity 1.5 kg
Payload Bay Configuration Ventral-mounted modular bay
Navigation System Built-in Dual RTK GNSS
Noise Level Below 65 dB
Ingress Protection IP54
Dual RTK The Dual RTK (Real-Time Kinematic) GNSS system represents precision navigation technology employing correction data from base stations to achieve centimeter-level positioning accuracy. Standard GPS provides 5-10 meter accuracy; RTK reduces this to 1-2 cm horizontally and 2-3 cm vertically—essential for precision mapping, photogrammetry, and infrastructure inspection applications.
RTK Accuracy ±0.01m
Flight Control Autonomous waypoint navigation
Communication Ground Control Station (GCS) with telemetry
Dimensions
Length 1.6 m
Height INA
Wingspan 2.6 m
Maximum Takeoff Weight 15 kg
Automotive
Engine Name T-MOTOR AT4130 KV230
Engine Type The T-MOTOR AT4130 KV230 represents a high-efficiency brushless motor optimized for VTOL applications.
Engine Power The KV230 rating indicates 230 RPM per volt—a relatively low KV value that provides high torque for VTOL lift while maintaining efficiency during cruise flight. The IP54 sealing protects internal electronics from dust ingress and water spray, enabling operations in adverse weather conditions.
Battery The platform utilizes Lithium Polymer (LiPo) battery technology—the predominant chemistry for electric UAVs due to high energy density and discharge rates. LiPo batteries employ solid polymer electrolytes rather than liquid, providing form-factor flexibility for airframe integration. The VF15E's battery configuration likely employs 6S (22.2V nominal) or higher voltage packs with 15,000+ mAh capacity based on endurance performance and comparable platforms.
Maximum Speed 110 km/h
Cruise Speed 75 km/h
Maximum Range 250 km
Service Ceiling 4,000 m
Endurance 210 minutes (3.5 hours) with 1.5 kg payload
Wind Resistance Level 6 (Beaufort scale) / 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
1.6 m
Width
2.6 m
Height
Weight
15 kg
Operators (1)
China
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