Russian compact unmanned helicopter by MAI's KB Iskatel for civil and special applications, valued for transportability. Single-rotor piston design; base for the larger Voron-333.
| 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 |
| Length (m) | 2.2 |
| Propulsion | Single piston engine (12 hp) |
| Combat-proven | No |
| Launch method | vertical take-off |
| Autonomy level | Autonomous flight capable |
| Recovery method | vertical landing |
| Max payload (kg) | 18 |
| Max speed (km/h) | 50 |
| Standard sensors | electro-optical / video payload |
| Production status | Developed / in use |
| Service ceiling (m) | 2100 |
| 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 |
| Signature / detectability | RCS – small |
| Speed regime | Medium (50–150 km/h) |
| Threat vector | Surveillance / reconnaissance |
| Weight / class | Class I – Small (20–150 kg), FAA >25 kg (Part 137 / waiver) |