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Lockheed Martin Polecat. Specifications. A photo.
Lockheed Martin Polecat. Specifications. A photo.

Lockheed Martin Polecat. Specifications. A photo.


Lockheed Martin Polecat - US military multipurpose unmanned aerial vehicle developed in 2005, the company «Lockheed Martin».

Design Lockheed Martin Polecat UAV model has been deployed by US aircraft manufacturers and experts in the field of aerospace systems and technologies in the early 2000-ies. The new device is intended to be used as an air reconnaissance means, however, thanks to the vast possibilities, the drone could also be used to carry out patrol and observation flights, the implementation of search and special missions, and even as an independent combat unit that provides a device is very broad in scope.


UAV PhotosLockheed Martin Polecat


Unmanned aerial vehicle Lockheed Martin Polecat model made its first test flight in 2005 year, and due to the fact that the project could prove to be highly effective and promising, the device has been improved by the implementation of specific tasks. Nevertheless, in December 2006 years, unmanned aerial vehicle crashed, and therefore on its creation program was temporarily minimized, however, has not been abolished, it points to the fact that work on the project can be continued in the near future.

Американский военный дрон Lockheed Martin Polecat обладает достаточно большими габаритами своего фюзеляжа, в частности, при длине 8 метров 30 сантиметров, размах крыльев БПЛА составляет 27 метров 44 сантиметра, что в некоторой степени ограничивает его манёвренность, однако, для минимизации этого негативного фактора, беспилотный летательный аппарат оснащён двумя мощными реактивными двигателями, каждый из которых обладает тяговой мощностью в 13,38 кН, суммарная работа которых позволяет дрону развивать максимальную скорость своего перемещения в 750 км\ч., в то время, как режим автономного полёта ограничен 4 часами.


Specifications Lockheed Martin Polecat.


  • Length: 8,3 m .;
  • Wingspan: 27,44 m .;
  • Height: 2,2 m .;
  • Maximum takeoff weight: 4100 kg .;
  • Cruising flight speed: 700 km \ h .;
  • Maximum flight speed: 750 km \ h .;
  • Maximum flight distance: 1500 km .;
  • Maximum flight height: 20000 m .;
  • aircraft engine Type: Jet;
  • Powerplant: 2 x Williams FJ44-3E;
  • Power: 2 x 13,38 kN.


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