Product overview
The aircraft uses hybrid propulsion and a fixed-wing design with vertical takeoff and landing.
Its maximum takeoff weight is 150 kg, and its maximum payload capacity is 50 kg including fuel.
The listed endurance is 10 hours; the record does not specify a load configuration for this figure.
The listed range is 850 km at a payload of 20 kg.
The aircraft can simultaneously carry an electro-optical gimbal, satellite communications equipment, public-network and PDT base stations, broadband ad hoc networking equipment and three-dimensional modeling equipment. These support emergency communications, data collection and disaster rescue when network access, power and roads are unavailable.
Specifications
| Specification | Value & conditions |
|---|---|
| Maximum takeoff weight | 150 kgMaximum listed in the product record. |
| Maximum payload capacity | 50 kgIncludes fuel. |
| Endurance | 10 hoursListed endurance. |
| Range | 850 kmAt a payload of 20 kg. |
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