Russian unmanned helicopter developed by MAI on the basis of the Voron-300 with revised design and improved characteristics. Single piston engine, for reconnaissance and monitoring.
| Country | Russia |
|---|---|
| Subtype | Unmanned helicopter (rotary-wing UAV) |
| Role | Reconnaissance / monitoring |
| Russian-made | true |
| Classification | Light rotary-wing UAV |
| Mission | reconnaissance, surveillance, monitoring, special purpose |
| Variants | Voron-300, Voron-333 |
| MTOW (kg) | 45 |
| Operators | Russia |
| Frame type | Helicopter / single-rotor |
| Propulsion | Single piston engine |
| Range (km) | 15 |
| Combat-proven | No |
| Launch method | vertical take-off |
| Autonomy level | Autonomous flight capable |
| Endurance (min) | 150 |
| Recovery method | vertical landing |
| Max payload (kg) | 18 |
| Max speed (km/h) | 150 |
| Standard sensors | electro-optical / video payload |
| Production status | Developed |
| Airframe / lift type | Single-rotor / helicopter |
| Control / autonomy level | Semi-autonomous (human-on-the-loop) |
| Domain | Aerial (UAV/UAS) |
| Mission / use case – military | ISR |
| Origin / supply chain | Military-grade |
| Propulsion | ICE – petrol |
| Range / endurance | Close range (5–50 km, 1–6 hrs) |
| Signature / detectability | RCS – small |
| Speed regime | High (150–400 km/h) |
| Threat vector | Surveillance / reconnaissance |
| Weight / class | Class I – Small (20–150 kg), FAA >25 kg (Part 137 / waiver) |