Russian multipurpose VTOL UAV complex of multi-rotor scheme, built from carbon fiber. VTOL from a small pad then transitions to forward flight. State tests began ~2014-2015 under the Russian MoD.
| Country | Russia |
|---|---|
| Subtype | VTOL multi-rotor UAV |
| Role | ISR |
| Russian-made | true |
| Class | Mini |
| Classification | Mini VTOL UAV |
| Mission | reconnaissance, surveillance, monitoring |
| Datalink | Remote control to 0.5 km; navigation to 40 km |
| MTOW (kg) | 5.5 |
| Operators | Russia |
| Frame type | VTOL hybrid |
| Propulsion | Electric |
| Range (km) | 40 |
| Launch method | vertical takeoff (VTOL) |
| Autonomy level | Autonomous waypoint with manual mode |
| Recovery method | vertical landing (VTOL) |
| Year introduced | 2017 |
| Max payload (kg) | 1.5 |
| Standard sensors | EO camera |
| Production status | Tested/limited |
| Combat radius (km) | 40 |
| Service ceiling (m) | 4000 |
| Airframe / lift type | VTOL hybrid – quadplane |
| Control / autonomy level | RC line-of-sight – VLOS, Semi-autonomous (human-on-the-loop), Waypoint / GPS-guided |
| Domain | Aerial (UAV/UAS) |
| Mission / use case – military | ISR |
| Origin / supply chain | Military-grade |
| Propulsion | Electric (LiPo / Li-ion) |
| Range / endurance | Close range (5–50 km, 1–6 hrs) |
| Signature / detectability | GNSS-dependent, RCS – small |
| Threat vector | Surveillance / reconnaissance |
| Weight / class | Class I – Mini (2–20 kg), FAA <25 kg (Part 107) |