Product overview
The droneyee ZY-GZ140 is a coaxial twin-rotor UAV system intended for individual deployment, vehicle coordination, air-drop deployment and military observation or strike roles. Its folding architecture supports portable carriage and rapid deployment, with handheld, launched and air-dropped operating modes. Folded length is ≤670 mm and diameter is ≤φ140 mm. Maximum takeoff weight is ≤13 kg including the warhead. It is presented as a flight system with control and networking functions; the described configuration includes an airborne networking module and operation with a matching docking station.
Payload integration supports electro-optical gimbals, communications base stations and warhead modules, with quick-release field replacement. Payload capacity is ≥5 kg, while endurance is 15 minutes with a 5 kg load or 30 minutes unloaded at normal temperature. Autonomous flight without GPS and continued flight during navigation failure or data-link interference are supported. With the Zhuoyi cloud platform, the system enables remote launch and recovery, multiple-terminal control and mission updates. Wind ratings conflict between Force 6 and Force 8; the technical specifications give Force 6.
Specifications
| Specification | Value & conditions |
|---|---|
| Product architecture | ZY-GZ140 coaxial twin-rotor UAV system. |
| Deployment modes | Handheld, launched and air-dropped deployment. |
| Portable configuration | Portable folding design with rapid deployment, mobile docking-station takeoff and landing, and support for high-speed air drops. |
| Flight speed | 100 km/h. |
| Wind resistance | Force 6; the technical specifications also give Force 6. |
| Additional wind-resistance rating | Force 8 is also stated, conflicting with the Force 6 rating. |
| Autonomous flight | Autonomous flight without GPS.Without GPS. |
| Mission automation | Target-guided strike capability under satellite denial, autonomous flight-route planning and swarm control.Satellite-denied conditions for target-guided strike capability. |
| Maximum takeoff weight | ≤13 kg.Including warhead. |
| Overall length | ≤670 mm.Folded configuration. |
| Diameter | ≤φ140 mm. |
| Payload | ≥5 kg. |
| Warhead payload statements | ≥5 kg; a repeated description additionally specifies greater than 5 kg.Effective warhead payload. |
| Strict warhead payload threshold | Greater than 5 kg.Effective warhead payload. |
| Maximum operational distance | ≥5 km. |
| Operational radius | Up to 5 km.With matching docking station. |
| Endurance | 15 min with 5 kg payload; 30 min unloaded.Normal-temperature conditions; 5 kg payload or no payload, respectively. |
| Maximum operating altitude | ≥4500 m.Altitude above sea level. |
| Maximum flight height | ≥1000 m.Relative height. |
| Climb rate | ≥5 m/s. |
| Descent rate | ≥5 m/s. |
| Maximum level-flight speed | ≥30 m/s.Level flight. |
| Flight continuity under interference | Can maintain flight during satellite-navigation failure and data-link interference.Satellite-navigation failure or data-link interference. |
| Networked control | Airborne network access, remote takeoff and landing, data acquisition and control from multiple terminals, cloud data processing and remote mission updates.Equipped with an airborne networking module and used with the Zhuoyi cloud platform. |
| Payload integration | Supports electro-optical gimbals, communications base stations and warhead modules, with quick-release replacement in the field. |
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