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High-Precision Rotor Head Control
The control drive servos and main avionics system are designed with high-sealing enclosures for IP65 protection standard, ensuring reliable operation even in harsh environments such as marine settings or light rain weather. The control linkage is constructed from full-metal stainless steel, offering excellent durability and weather resistance. -
Composite Matrix-Structured Airframe
The main airframe structure is constructed using high-strength aluminum alloy and carbon fiber composite materials, assembled with a matrix-style configuration for stability. This design not only facilitates easy assembly and maintenance, but also allows for secure and quick battery installation and removal, accommodating various battery formats. -
Direct-Drive Enclosed Gearbox
Fully sealed gearbox offers excellent protection, enhancing the reliability and durability of the transmission system. It features an optimized gear ratio design, paired with high-carbon alloy steel gears ensuring power delivery from the motor to the main and tail rotors (motor:main rotor:tail rotor) is 6:1:1.
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Streamlined Array-Structured Airframe
The main airframe structure features a streamlined array-based layout, designed for easy assembly and maintenance. For storage and transportation, the main rotor can be folded backward and secured onto the tail rotor mounting plate, significantly reducing the overall size of the aircraft and allowing it to be conveniently stored in a transport case.
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Power Control Module
Equipped with an electric propulsion system offering low noise and low vibration performance, hovering over targets and enhancing operational stealth. Integrated GPS data logging enables precise location tracking & supporting data collection. Real-time transmission to the command intelligence center is made possible through onboard communication systems. -
Payload Release Mechanism
A servo-controlled hook or mechanism is integrated into the rear landing gear, enabling the deployment of additional payloads and remote delivery within the maximum takeoff weight limit. This design maintains the aircraft's center of gravity and stable flight without requiring additional counterweights.

Design And Performance

Flight Control

Imaging System

Special Features
Electric propulsion ensures low noise and improve concealment during hovering. Built-in GPS logging enables accurate positioning, supports image focus, and enables real-time data transmission to the intelligence center.

Application Fields
Overall Length | 1890mm |
Overall Width | 400mm |
Overall Height | 570mm |
Main Rotor Diameter | Ф2315mm |
Tail Rotor Diameter | Ф360mm |
Maximum Takeoff Weight" (MTOW) | 30kg |
Aircraft Empty Weight (excluding battery) | 11 kg |
Total Battery Weight | 11.5 kg |
Basic Payload Weight (dual-sensor gimbal + communication link) | 2.9kg |
Maximum External Payload Weight | 4.6 kg |
Maximum Cruise Speed | 85Km/hr |
Maximum Operating Altitude | 500m |
Maximum Endurance Time (with basic payload) | >60min |
Basic Control Communication Range | ≧30Km |
Wind Resistance | Up to Beaufort Scale 6 (inclusive) |
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Ground Control Station System
6 degrees Freedom MEMS sensor, 3 axis magnetometer, GNSS receiver supporting GPS/GLONASS dual positioning, and a high-precision SINS/GPS inertial navigation system. Supports real-time telemetry, automatic RTL and hovering for safety & stability. -
Gimbal System
Features a detachable 3-axis EO/IR gimbal camera with high-definition visible and thermal imaging. Quick-mount slide design with shock absorption ensures stable image quality. Smart tracking module allows PTZ control via GCS software. -
Dual-Band Wireless Communication
Integrates data and video transmission modules in a lightweight waterproof metal housing. Designed for rugged use with easy installation via sliding rails. Supports ISM bands and customizable frequency and power configurations.
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Ground Control Station System
Military-grade sealed case, integrating transmission module for real-time communication with the UAV autopilot with recordings saved to the computer. Industrial-grade high-brightness display for live video feeds and a control panel with flight controller and dual joysticks for manual operation. Built-in GCS software supports automated mission planning and map data. -
Charger
Designed for two 6-cell lipo batteries, supporting multiple operating modes including balance charging & storage mode with user-friendly interface, also featuring a master-slave configuration enabling synchronized settings across multiple units via data cable connection. Short circuit protection, reverse polarity & over-temperature protection are available. -
Battery
The battery system is built around lithium polymer cells, offering high energy density, fast charging, excellent safety, long endurance, and high cycle life. Its strong stability makes it ideal for electric UAVs and other demanding applications. The batteries are certified to IEC-62133 standards by a TAF-accredited testing body.

AXH-E230IIC Certification Mode

AXH-E230D Motor Direct Drive
Utilizing high-torque brushless motors and direct-drive rotors eliminates traditional gear & belt transmissions, enhancing power efficiency and reducing maintenance costs. The inherent low-vibration and high-stability characteristics of direct-drive helicopters ensure long-duration flight, making them ideal for defense reconnaissance.

AXH-E230FC Hydrogen Fuel System

AXH-E230RS CG Edition

AXH-E230ST "Capricorn" Tactical UAV
