Product overview
The aircraft supports small-scale surveying, power inspection and farmland monitoring.
Its listed maximum take-off weight is 13.5 kg, with a payload of 3 kg.
The published specifications state an all-electric endurance of up to 240 min and a practical ceiling of 5000 m.
A carbon fiber fuselage and electric pusher propulsion accompany modular mission payload support. Assembly and disassembly are listed at 3 min.
Standard RTK differential positioning provides stated centimeter-level accuracy, and the aircraft supports equipment such as multispectral cameras.
Specifications
| Specification | Value & conditions |
|---|---|
| Maximum take-off weight | 13.5 kgPublished maximum take-off weight for the selected aircraft. |
| Payload | 3 kgPublished payload. |
| Endurance | Up to 240 minAll-electric operation. |
| Practical ceiling | 5000 mPublished practical ceiling. |
| Assembly and disassembly | 3 minPublished quick assembly/disassembly time. |
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