Yakovlev Pchela

Source: Wikipedia, the free encyclopedia.
Pchela
Pchela-1T UAV on a starting ramp (closeup view)
Role
Unmanned air vehicle
National origin Soviet Union/Russia
Manufacturer Yakovlev
First flight 1986
Primary user Russian Air Force

The Yakovlev Pchela-1T ("Пчела" meaning

downlinked
video. Other implementations and uses include target designation and as a training target.

Design

Pchela-1T UAV on a BTR-D launcher

The Pchela is launched using rocket assist by two

solid-propellant booster rocket engines, and it is recovered via parachute. The Pchela-1T has a range of 60 km (37 mi), flies at 100–2,500 m (330–8,200 ft) altitude at 120–180 km/h (75–112 mph). The maximum takeoff weight
for the vehicle is 138 kg (304 lb). Yakovlev lists the vehicle endurance at two hours.

Operators

References

  1. ^ The Military Balance 2016,p.190
  2. ^ The Military Balance 2016,p.266
  3. ^ "Внутри тайной программы БПЛА Северной Кореи « TodaysMilitary. Информатор о военных действиях". Archived from the original on 2017-06-30. Retrieved 2016-08-20.

External links