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The CD140 is a high-performance folding-wing UAV designed for rapid deployment and multi-role mission capabilities. It features excellent endurance and operational flexibility, with a foldable wing design for easy storage and efficient deployment. Integrating information acquisition and precision strike capabilities, it adapts to complex combat environments, supports individual soldier carry and multi-platform integrated launch, enabling rapid response and accurate disposal of various targets, serving as a vital equipment platform for modern informatized operations.
CD180 UAV System Overview
The CD180 UAV System is an integrated mission system combining the aerial vehicle and the ground control station, achieving full-process mission management and support:
Aerial Vehicle: Integrates a high-stability flight platform, high-precision mission payloads, and multi-purpose mission equipment to support
diverse operational scenarios.
Ground Control Station: Equipped with professional ground TT&C terminals and launch support devices to complete UAV mission planning, real-time control, and full-process support.
Core System Features
1. Adopts pneumatic portable launch method for rapid deployment.
2. Modular structure design allows quick refitting and adaptation of mission payloads.
3. Equipped with real-time target acquisition capability for high- precision strikes.
4. Simplified operation process
greatly reduces personnel training cycle and usage costs.
Core Technical Specifications
| No. | Specification | Value |
|---|---|---|
| 1 | Endurance | ≥180 mins, supporting long-duration missions |
| 2 | Max Takeoff Weight | 18kg, compatible with various payloads |
| 3 | Payload | ≥5kg, for diverse mission equipment |
| 4 | Service Ceiling | 3000m, adapting to different airspace |
| 5 | Folded Size | ~1675mm long, excellent portability |
| No. | Specification | Value |
|---|---|---|
| 1 | Max Speed | ≥45m/s, rapid penetration capability |
| 2 | Min Turning Radius | ≤170m, flexible maneuverability |
| 3 | Mission Altitude | 50m–2000m, multi-airspace coverage |
| 4 | Guidance | Visible/IR dual-mode for all-weather tracking |
| 5 | Data Link | 50/100km, -20℃~+45℃ resistant |
| 6 | Recovery | Parachute for system reuse |
CD180 UAV Platform Overall Architecture
Aerodynamic Layout and Structural Design
Basic Design: The CD180 UAV platform adopts a highly reliable conventional aerodynamic layout, achieving a perfect balance between aerodynamic efficiency and mission payload compatibility. The fuselage is constructed from lightweight composite materials, and the wings have excellent lift-to-drag ratio characteristics, physically ensuring the platform's flight stability and energy efficiency.
Physical Craft and Payload Adaptation
Multi-mission Adaptation:The platform reserves standardized, multi- dimensional payload interfaces, which can flexibly adapt and integrate various mission equipment such as EO/IR electro-optical reconnaissance, synthetic aperture mapping radar, and communication relays, providing solid and reliable hardware support for long- endurance patrols, complex terrain mapping, emergency communication support and other multi-scenario operations.
CD180 UAV Ground Control Terminal System
As the core hub for UAV command and control, this system can decode real-time airborne HD video and precise flight data, realizing integrated control of UAV track planning, attitude adjustment, and mission payloads (EO/IR, gimbal cameras, etc.). For different application scenarios, it provides a dual hardware adaptation solution of handheld terminals and semi-rugged notebooks, balancing portability and professionalism.
Handheld Terminal
Adopting a lightweight and portable design, it adapts to the needs of rapid field deployment and has drop- proof, dust-proof, and waterproof properties. It supports key commands such as one-click takeoff and emergency return, meeting the requirements for immediate control and rapid response in complex outdoor environments.
Semi-rugged Notebook
Adopting a ruggedized chassis structure, equipped with a high-resolution display and full-function keyboard, it is suitable for command centers and vehicle-mounted mobile command scenarios. It can support complex business processing such as multi-UAV collaborative scheduling and mission data review and analysis.
CD180 UAV System Key Components
TT&C Communication Link
A point-to-point wireless image and data transmission product specially designed for UAV applications, built on OFDM technology, with multi-channel, high-speed, low-latency, anti- jamming, and long-distance communication capabilities.
Multiple specifications of 20km, 50km, and 100km can be flexibly configured according to mission requirements to ensure stable and reliable data transmission.
TT&C Core Module
Portable Pneumatic Launch Tube
Adopting a portable launch tube design, the UAV is accelerated and launched by high-pressure gas generated by a built-in gas generator. It has a large-caliber structure (inner diameter φ216mm, outer diameter φ218mm, total length 2100mm) and adopts a separable architecture, supporting both single-soldier independent use and integration into other carrier platforms, adapting to future multi-platform collaborative combat needs.
Pneumatic Launch Device
EO/IR Payload (Optional)
High-performance EO/IR composite payloads can be flexibly configured according to the actual needs of different mission scenarios to accurately meet the requirements of diverse battlefield reconnaissance, target observation, and situational awareness tasks.
Multispectral Reconnaissance Payload
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