Product overview
The JOUAV CW-30E is a hybrid gasoline-and-battery aircraft combining fixed-wing architecture with vertical takeoff and landing for land and maritime missions. Gasoline and heavy-fuel configurations are available. Its fuselage measures 2.4m, its wingspan measures 4.4m, and its maximum takeoff weight is 38kg. Payload configuration can be customized to mission needs. This is a UAV flight platform with integrated flight control and navigation, and its maritime functions include takeoff and landing from a mobile platform.
Automatic pre-flight checks, automatic task execution and emergency automatic return support the operating workflow. The aircraft incorporates a self-heating airspeed tube and battery for operation in high altitude, high humidity, low temperature and light rain conditions. With JOUAV EagleMap, operators can use mission planning, video surveillance, real-time mosaic, multi-station networking and remote takeoff and landing.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | JOUAV CW-30E |
| Architecture and purpose | VTOL fixed-wing UAV for land and maritime missions |
| Power architecture | Hybrid gasoline and battery |
| Fuel configurations | Gasoline and heavy-fuel configurations |
| Fuselage | 2.4m |
| Wingspan | 4.4m |
| Maximum takeoff weight | 38kg |
| Maximum payload | 8kgTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Maximum flight time | 480minTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Cruising speed | 90km/hTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Wind resistance | 13.9-17.1m/sTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Maximum service ceiling | 6000mTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Maximum takeoff altitude | 3500mTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Takeoff and landing | VTOL |
| Vertical positioning accuracy | 3cmTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Horizontal positioning accuracy | 1cm+1ppmTheoretical laboratory performance under particular conditions; actual performance varies with product configuration, software versions, application conditions and environmental factors. |
| Configuration customization | Customizable payload configuration |
| Automatic functions | Automatic pre-flight check, automatic task execution and emergency automatic return |
| Environmental equipment | Self-heating airspeed tube and batteryHigh altitude, high humidity, low temperature and light rain. |
| Maritime takeoff and landing | Supports mobile-platform takeoff and landingMobile platform. |
| Mission software functions | Mission planning, video surveillance, real-time mosaic, multi-station networking and remote takeoff and landingUsing JOUAV EagleMap. |
| Performance measurement qualifications | Theoretical laboratory values; actual performance varies with product configuration, software versions, application conditions and environmental factors.Performance measurements obtained under particular laboratory conditions. |
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