Experimental multipurpose VTOL/V-STOL fixed-wing turbojet UAV by the INDELA design laboratory (Minsk); the Shtil-3 sample was presented at MAKS-2005. A small ~24 kg aircraft using three turbojet engines (two tilting main turbines plus a hover pilot engine) with a radio-transparent airframe; performs vertical takeoff/landing and high-speed horizontal flight.
| Country | Belarus |
|---|---|
| Subtype | V/STOL UAV |
| Role | Reconnaissance |
| Class | Mini |
| Classification | Experimental V/STOL turbojet UAV |
| Mission | Reconnaissance |
| Variants | Shtil-3 |
| Notable partners | KVAND |
| MTOW (kg) | 24 |
| Frame type | Tiltrotor |
| Propulsion | Turbojet |
| Launch method | VTOL |
| Autonomy level | Semi-autonomous |
| Endurance (min) | 140 |
| Recovery method | VTOL |
| Year introduced | 2005 |
| Max speed (km/h) | 780 |
| Production status | Prototype |