Product overview
The aircraft is intended for surveying and mapping, power inspection and farmland monitoring.
Its stated maximum takeoff weight is 20 kg, with a payload of 6 kg.
Pure electric endurance is stated as up to 330 min.
The aircraft uses an electric pusher configuration and a carbon fiber fuselage. It has a separate, replaceable camera compartment and standard RTK/PPK differential positioning.
Specifications
| Specification | Value & conditions |
|---|---|
| Maximum takeoff weight | 20 kgStated maximum takeoff weight for the aircraft. |
| Payload | 6 kgStated payload. |
| Endurance | Up to 330 minPure electric operation. |
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