| Country | Israel |
|---|---|
| Airframe / lift type | Multirotor – quad |
| Control / autonomy level | Fully autonomous (human-off-the-loop, AI-navigated) |
| Domain | Aerial (UAV/UAS) |
| Mission / use case – civil | Inspection |
| Propulsion | Electric (LiPo / Li-ion) |
| Range / endurance | Very close range (<5 km, <1 hr) |
| Signature / detectability | GNSS-dependent, RF-emitting |
| Weight / class | Class I – Mini (2–20 kg), FAA <25 kg (Part 107) |
| Confidence | low |