Product overview
The HAWKUN INTELLIGENCE P22 is an electric flight platform for large-area missions, combining multirotor vertical take-off and landing with fixed-wing flight. Its modular composite fuselage measures 1950mm×3800mm×525mm, with a take-off weight of 22kg and a maximum load of 5kg. Different mission payloads can be fitted according to the task. The battery configuration is two 6S 22.8V 32000mAh lithium polymer batteries. Cruise speed is 25m/s (90km/h), maximum speed is 37m/s (133km/h), and maximum endurance is ≥210min. Take-off and landing require an 8×8m site.
The flight-control configuration supports autonomous take-off and landing, in-flight waypoint changes, and mission continuation after a battery replacement following a low-battery or weather-related return. During fixed-wing flight, stall or loss of attitude control triggers multirotor assistance. Navigation combines GPS, BeiDou and GLONASS bands with PPK post-differential positioning. Ground station software runs on ordinary computers or notebooks and checks planned survey routes for terrain clearance, flagging sections that require altitude adjustment. Operating limits include a temperature range of -20 to 45°C, wind resistance of 12.5m/s, and light-rain resistance limited to rainfall ≤10mm/24h.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | HAWKUN INTELLIGENCE P22 |
| Product type and purpose | Pure electric VTOL fixed-wing UAV for large-area missions, configurable with different mission payloads. |
| Fuselage construction | Composite-material fuselage with a modular structure. |
| Take-off and landing mode | Multirotor vertical take-off and landing |
| Flight mode | Fixed-wing mode |
| Cruise and maximum speed | Cruise speed: 25m/s (90km/h); maximum speed: 37m/s (133km/h) |
| Take-off weight | 22kg |
| Maximum load | 5kg |
| Ceiling | ＞5000m |
| Dimensions | 1950mm×3800mm×525mm |
| Navigation satellite | GPS: L1+L2, BeiDou: B1+B2, GLONASS: L1+L2 |
| Differential mode | PPK post-differential |
| Landing accuracy | Horizontal ≤±0.3m, elevation ≤±0.3m |
| Wind resistance | 12.5m/s |
| Operating temperature | -20~45℃ |
| Maximum endurance | ≥210min |
| Rain resistance | Light rain (rainfall ≤ 10mm/24h)Rainfall ≤ 10mm/24h. |
| Take-off and landing site | 8*8m |
| Battery | 6S 22.8V 32000mAh*2 lithium polymer battery |
| Autonomous take-off and landing | Fully autonomous take-off and landing. |
| Multirotor flight assistance | Flight control automatically activates the multirotor system for auxiliary flight.During fixed-wing flight, if stall or loss of attitude control occurs. |
| Mission continuation | Automatically resumes remaining missions without replanning.After a return caused by low battery or weather and subsequent battery replacement. |
| Dynamic waypoint control | Supports waypoint changes, waypoint skipping, and mission pauses with hovering.During flight. |
| Flight data recorder | Built-in flight data recorder with recording time exceeding 100 hours.When recording space is insufficient, old data is automatically deleted. |
| Ground station computer | Ground station software can operate on ordinary computers or notebooks. |
| Route terrain checking | Automatically checks terrain clearance and displays a red danger warning where the planned route is too close to the ground, requiring altitude adjustment.After an aerial survey mission plan is generated. |
