Product overview
The aircraft uses a hybrid power design and a blended wing-body aerodynamic layout.
The published maximum mission payload is 40 kg, and maximum endurance is 10 hours.
The flight-control system uses two hot-backup flight controllers, each independently integrated and powered. An onboard bus network enables real-time data sharing between them.
Specifications
| Specification | Value & conditions |
|---|---|
| Maximum mission payload | 40 kg |
| Maximum endurance | 10 hours |
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