V500 . Features
V500 adopts hybrid power, with streamlined high-aspect-ratio wings and wing-body integrated layout, and can achieve 10h of endurance. Meanwhile, V500 is equipped with a fully automatic takeoff and vertical takeoff and landing system and can be additionally equipped with a high-precision stable photoelectric platform. The UAV is featured by fully autonomous operation, providing users with more convenient and reliable operations, more flexible application and more simplified operation threshold.
Ultimate Performance: 10h super-long endurance+13kg maximum payload. It adopts highly cambered blade, high lift coefficient, and be suitable for prolonged hanging.
- Quick Response : Disassembly and assembly can be completed in 15 min without any tool and multiple mission payload can be customized.
- Low Threshold: With a fully autonomous operating system, enabling simpler operation.
| Specification | |
| Aircraft | |
| Length | 256cm |
| Span | 494cm |
| High | 90cm |
| Model | Hydro-powered vertical take-off and landing fixed wing |
| Body material | Composite materials fiberglass and carbon fiber |
| Maximum payload | 20kg (including oil) |
| Maximum flight speed | 110km/h |
| Cruising speed | 85km/h |
| Stall speed | 61km/h |
| Maximum takeoff altitude | 4500m |
| Maximum takeoff weight | 60kg |
| Battery life | 10h (load 3kg) |
| Maximum flight distance | 1000km |
| Minimum circle radius | 100m |
| Navigation mode | GPS/GLONASS/Beidou |
| Wind resistance | Level 6 wind |
| Range of working temperature | -10℃~ +60℃ |
| Takeoff mode | Vertical takeoff |
| Landing mode | Vertical landing |
| Ceiling | 6000m |
| Deployment time | 20min |
| Protection level | IP43 |
| Packing box size | 260*68*95cm |
| Engine Parameters | |
| Weight, kg | 5.8 |
| Peak output electrical power, kw | 8.9 |
| Rated speed, rpm/min | 6000 |
| Fuel tank capacity, L | 18 |
| Cooling method | Air cooling |
| Throttle control | PWM |
| Fuel injection method | EFI |
| Gasoline label | 92 |
| Oil grade | 2 strokes of engine oil |
| Oil to gasoline mixture ratio | 1:40 |
| Average fuel consumption, L/h | 1.3 |
| Adaptation voltage, v | 24 |
| Start and stop mode | Electric start |
| Bus communication | TTL |
| Configuration | ||
| PnP | RTF | |
| Fuselage | 1 | 1 |
| Wings | 2 | 2 |
| Tails | 2 | 2 |
| Vertical Fins | 2 | 2 |
| Landing Gears | 2 | 2 |
| Propellers | 4+1 | 4+1 |
| Flight Control | 1 | 1 |
| Motors | 4+1 | 4+1 |
| Gasoline Engine | 1 | 1 |
| Steering Engine | 2 | 2 |
| ESC | 4+1 | 4+1 |
| Fuel Tank | 1 | 1 |
| Battery | 9 | |
| Charger | 1 | |
| Receiver | 1 | |
| Transmitter | 1 | |
| Remote Controller | 1 | |
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