Product overview
The aircraft uses an air-cooled fuel cell system independently developed by its maker.
The published maximum takeoff weight is 25 kg, and the maximum payload is 5 kg.
The stated endurance is 2 hours.
The aircraft has six rotors and a whole-aircraft parachute, with a structure designed for quick assembly and disassembly.
It supports different payload pods for transportation, power grid, forestry, emergency response and surveying work.
Specifications
| Specification | Value & conditions |
|---|---|
| Maximum takeoff weight | 25 kgPublished maximum for this aircraft. |
| Maximum payload | 5 kg |
| Claimed endurance | 2 hours |
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