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

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 edit

See also edit

Aircraft of comparable role, configuration, and era

References edit

  1. ^ "MTI Pegaz project page". MTI.
  2. ^ "Vojska Srbije počela koristiti Pegaze, evo što sve znamo o borbenim dronovima nastalim u suradnji s Kinezima". tportal.hr. Retrieved 2023-03-03.

External links edit