Product overview
The Lyncon Technology GHQ-600 combines a twin-boom airframe, high-aspect-ratio high wing and rear-mounted pusher engine. Its four-cylinder, four-stroke piston powerplant supports a platform intended for substantial payloads and extended missions. Dedicated flight-control and navigation systems provide autonomous flight from an operator-submitted flight plan, including wheeled runway takeoff and landing. Maximum takeoff weight is 680kg and maximum payload is 180kg. Endurance depends on loading: 17h unloaded, 10h with 130kg and 9h at full payload.
Payload integration covers cloud water-content detectors, cloud particle spectrometers and flare dispensers for meteorological work, alongside logistics and delivery applications. Additional electrical power is ≥2kW. Both listed sensing instruments measure 130mm×153mm×212mm, weigh 1.1kg and consume ≤30W normally, with ≤150W peak consumption. Anti-icing and whole-aircraft parachute recovery are described as optional in the platform description, although the safety features also describe them as fitted. Flight-control and link equipment use multiple redundancy. Operating limits include -40°C to 55°C, moderate rain and Force 8 wind resistance.
Specifications
| Specification | Value & conditions |
|---|---|
| Product type and purpose | Lyncon Technology GHQ-600 high-payload, long-endurance fixed-wing UAV flight platform. |
| Airframe and propulsion architecture | Twin-boom airframe with a high-aspect-ratio high wing and a pusher four-cylinder, four-stroke piston engine. |
| Flight control and navigation | Integrated dedicated flight-control and navigation systems support fully autonomous flight using an operator-submitted flight plan. |
| Payload integration | Can accommodate meteorological equipment including a cloud particle spectrometer, cloud water-content detector and flare dispenser. |
| Safety equipment configuration | Anti-icing and parachute recovery systems are available as optional equipment.Anti-icing and parachute recovery are described as optional in the platform description and as fitted in the safety features. |
| Avionics redundancy | Flight-control, communications-link and other onboard equipment use multiple redundancy. |
| Maximum takeoff weight | 680kg |
| Maximum payload capacity | 180kg |
| Endurance without payload | 17hUnloaded. |
| Endurance with 130kg payload | 10h130kg payload. |
| Endurance at full payload | 9hFull payload. |
| Maximum flight speed | 255km/h |
| Cruise speed | 120–200km/h |
| Maximum takeoff elevation | 4400m |
| Service ceiling | 8000m |
| Additional electrical power | ≥2kW |
| Wind resistance | Force 8 |
| Rain capability | Moderate rain |
| Operating temperature | -40°C to 55°C |
| Takeoff and landing requirement | Fully autonomous wheeled takeoff and landing.Wheeled runway takeoff and landing. |
| Runway length | Can take off and land on a runway no longer than 800m.Runway takeoff and landing. |
| Cloud water-content detector dimensions | 130mm×153mm×212mmAirborne cloud water-content detector. |
| Cloud water-content detector weight | 1.1kgAirborne cloud water-content detector. |
| Cloud water-content detector power consumption | Normal: ≤30W; peak: ≤150WAirborne cloud water-content detector; normal and peak consumption respectively. |
| Cloud particle spectrometer dimensions | 130mm×153mm×212mmCloud particle spectrometer. |
| Cloud particle spectrometer weight | 1.1kgCloud particle spectrometer. |
| Cloud particle spectrometer power consumption | Normal: ≤30W; peak: ≤150WCloud particle spectrometer; normal and peak consumption respectively. |
| Applications | Weather modification, logistics transport support and transport delivery. |
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