The reinforced fuselage and chassis are designed for tough landing on unpaved airfields and prepared sites. The UAV can serve as a platform for a payload of up to 200 kg and has an operating time of up to 24 hours, depending on the altitude and operating conditions.
Parameter | Value |
---|---|
Max Take Off Weight (MTOW) | 550 kg |
Max cruising speed | 200 km/h |
Max speed | 218 km/h |
Endurance | 24 hours |
Stall speed | 65 km/h |
Takeoff run distance – 0 m/s wind | 450 m |
Landing run distance – 0 m/s wind | 600 m |
Wingspan | 15 m |
Fuselage length | 6.5 m |
Fuselage height | 1.82 m |
Engine | Rotax 912iS |
Engine power | 100 HP |
Fuel consumption, cruising speed | 12.1 l/h |