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The BPL Pegaz 011 is a tactical unmanned aerial vehicle prototype developed at the Military Engineering Institute, premiered at the 2011 Partner Arms Fair.
Pegaz in 2011
Serbian UAV
Specifications
Data from MTI Pegaz project page
[1]
General characteristics
Capacity: 50 kg (110 lb) payload
Length: 5.395 m (17 ft 8 in)
Wingspan: 7.025 m (23 ft 1 in)
Height: 1.6 m (5 ft 3 in)
Wing area: 4.24 m2 (45.6 sq ft)
Empty weight: 120 kg (265 lb)
Max takeoff weight: 245 kg (540 lb)
Propellers: 2-bladed pusher propeller
Performance
Maximum speed: 160–180 km/h (99–112 mph, 86–97 kn)
Cruise speed: 130–150 km/h (81–93 mph, 70–81 kn)
Range: 250 km (160 mi, 130 nmi) exact maximum range is yet unknown
Endurance: 6-10+ hours
Service ceiling: 6,000 m (20,000 ft)
Armament
Rockets: 2x FT-8D laser guided rocket
Avionics
Automatic takeoff from prepared runway (optional: catapult)
Automatic landing on prepared runway (emergency: parachute)
Fully autonomous way points tracking, holding, camera guiding Emergency and return home mode Altitude and velocity autopilot
Operators
See also
Aircraft of comparable role, configuration, and era
References
External links
Wikimedia Commons has media related to
Pegaz UAV .