Product overview
JOUAV Multirotor Hangar packages the PH-10H quadcopter, JOS-P200 docking station and JoCloud platform into an automated flight system for security, inspection and emergency response. Its architecture links aircraft operations to a station that swaps batteries and manages recharging, while JoCloud provides mission planning, data access and AI-assisted insights. The system components and reference payload arrangements, but those descriptions should be checked against the selected procurement configuration when specifying included equipment.
Installation planning needs to accommodate both the closed enclosure and its opened footprint. JOUAV publishes dimensions of 1.7 × 1.5 × 2.2 m closed and 3.2 × 1.5 × 1.8 m opened, with station weight below 249 kg including the stated two-hour UPS provision; confirm these values for the selected configuration. The station supports fixed-site or vehicle-mounted deployment, uses AC 220 V at 50 Hz, and provides Ethernet and fiber interfaces alongside cellular connectivity. Climate control and environmental monitoring support unattended operation.
Aircraft integration centers on a published 6 kg payload capacity and provision for up to four simultaneous payloads. Reference endurance is 48 minutes with a gimbal camera, loudspeaker and searchlight, or 43 minutes when a parachute is added; the broader 35–60-minute range depends on payload configuration. LiDAR, millimeter-wave radar and dual-lens vision provide sensing and positioning. Procurement requirements should retain the distinction between Level 6 operating winds and Level 8 emergency-landing winds. All performance figures carry JOUAV’s laboratory-condition and actual-use qualifications.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer, model and system configuration | JOUAV Multirotor Hangar: PH-10H drone, intelligent docking station and JoCloud platform; a complete flight-platform system.System composition. |
| Product purpose | Automated drone missions for security, inspection and emergency response.Applications. |
| Installation options | Fixed-site or vehicle-mounted deployment.Deployment options; confirm installation requirements for the selected configuration. |
| First launch time | Less than 1 minute from command receipt to first launch.Performance data are theoretical laboratory values under particular conditions; actual results depend on configuration, software, application and environment. |
| JOS-P200 closed dimensions, W × L × H | 1.7 × 1.5 × 2.2 m [5.6 × 4.9 × 7.2 ft], closed.Closed docking station. Dimensions. |
| JOS-P200 opened dimensions, W × L × H | 3.2 × 1.5 × 1.8 m [10.5 × 4.9 × 5.9 ft], opened.Opened docking station. Dimensions. |
| JOS-P200 operating temperature | −30°C to +50°C, with built-in climate control.With built-in climate control. Actual performance varies with configuration and operating conditions. |
| JOS-P200 power supply | AC 220 V, 50 Hz. |
| JOS-P200 drone battery recharge method | Battery swapping. |
| JOS-P200 second deployment time | Less than 1.5 min.Second deployment. Performance data are theoretical laboratory values under particular conditions; actual results may vary. |
| JOS-P200 maintenance interval | Once every 6 months. |
| JOS-P200 external communication interfaces | 1000M network and optical fiber. |
| Cellular connectivity | 4G/5G connectivity alongside Ethernet and fiber optic interfaces.Connectivity. And network provision. |
| JOS-P200 monitoring and outage response | Real-time air-pressure, temperature, humidity, wind-speed and rainfall monitoring; live video feed; automatic backup-battery switchover during outages.Functions. |
| JOS-P200 weight and UPS provision | Less than 249 kg, with 2 hours of UPS power.Weight includes UPS provision stated for 2 hours. Actual backup duration depends on operating conditions. |
| PH-10H operating altitude | 5000 m [16404.2 ft].Performance data are theoretical laboratory values under particular conditions; actual results may vary. |
| PH-10H maximum flight time, three payloads | 48 min.Standard three-payload configuration: gimbal camera, loudspeaker and searchlight. Theoretical manufacturer laboratory value; actual endurance varies with configuration, software, application and environment. |
| PH-10H maximum flight time, four payloads | 43 min.Four-payload configuration: gimbal camera, loudspeaker, searchlight and parachute. Theoretical manufacturer laboratory value; actual endurance varies with configuration, software, application and environment. |
| PH-10H flight-time range | 35–60 min.Depends on payload configuration. Theoretical manufacturer laboratory values; actual endurance varies with configuration, software, application and environment. |
| PH-10H maximum payload capacity | 6 kg; supports multiple-payload combinations.Actual performance depends on payload arrangement and operating conditions. |
| PH-10H simultaneous payload provision | Up to four simultaneous payloads, with cameras, loudspeakers, searchlights, parachutes and sensors cited as options.Payload integration. And included equipment. |
| PH-10H maximum flight speed | 16 m/s [31.1 kts].Performance data are theoretical laboratory values under particular conditions; actual results may vary. |
| PH-10H communication range | 15 km [9.32 mi], extendable with a cellular network module.Range is stated as extendable with a cellular network module. Theoretical manufacturer laboratory value; actual range depends on configuration and operating conditions. |
| PH-10H operating temperature | −30°C to +50°C.Performance data are theoretical laboratory values under particular conditions; actual results may vary. |
| PH-10H operational altitude | 5000 m [16404.2 ft].Separately repeated in the manufacturer's specification table. Actual performance varies with configuration and operating conditions. |
| PH-10H wind resistance and rain protection | Normal operation in winds up to Level 6; safe emergency landing in Level 8 winds; moderate-rain protection.Level 6 applies to normal operation; Level 8 applies to safe emergency landing. Rain protection is stated for moderate rain. Theoretical manufacturer laboratory values; actual performance may vary. |
| PH-10H obstacle sensing and positioning | Surround-view LiDAR, rear and downward millimeter-wave radars, and dual-lens vision positioning.Sensor architecture. |
| JoCloud mission and data functions | Flight planning and management, real-time data access and AI-assisted insights.Software functions. And service provision. |
| Manufacturer performance qualification | Published performance figures are theoretical values from JOUAV internal laboratory tests under particular conditions.Applies to all published performance figures; testing conditions are not fully. |
| Configuration and operating limitations | Actual performance depends on individual configuration, software version, application conditions and environmental factors.All data remain subject to actual usage. |
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