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Pegaz

From Wikipedia, the free encyclopedia

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

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See also

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Aircraft of comparable role, configuration, and era

References

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  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.
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