To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.

Lockheed Martin Polecat

From Wikipedia, the free encyclopedia

LM Polecat.jpg
A picture of the Lockheed-Martin Polecat released at the Farnborough Airshow in 2006
Role Unmanned aerial vehicle
Manufacturer Lockheed Martin Skunk Works
First flight 2005
Retired December 18, 2006
Number built 1
Developed from Lockheed Martin X-44 (UAV)
Developed into Lockheed Martin RQ-170 Sentinel

The Lockheed Martin Polecat (company designation P-175) was an unmanned aerial vehicle by Lockheed Martin. It was developed by the company's Advanced Development Programs division in Palmdale, California.

YouTube Encyclopedic

  • 1/3
    48 725
    2 431
    16 218
  • Lockheed Martin Unmanned Systems
  • MPUAV (multi-purpose UAV) by Skunk Works / Lockheed Martin - 2012 concept
  • Lockheed Martin MPUAV Cormorant


Design and development

Designated P-175, the Polecat was funded internally by Lockheed Martin (as opposed to using United States Government funds) at the beginning of 2005. The prototype was unveiled at the 2006 Farnborough Airshow.[1][2] It was developed over a period of 18 months.[3]

On December 18, 2006, the aircraft crashed due to an "irreversible unintentional failure in the flight termination ground equipment, which caused the aircraft's automatic fail-safe flight termination mode to activate."[4]


General characteristics

  • Crew: 0
  • Capacity: 1,000 lb (450 kg) of weapons or sensors
  • Wingspan: 90 ft 0 in (27.44 m)
  • Gross weight: 9,000 lb (4,082 kg)
  • Powerplant: 2 × Williams FJ44-3E turbofan engines, 3,010 lbf (13.38 kN) thrust each


  • Endurance: 4 hours
  • Service ceiling: 65,000 ft (20,000 m)


This page was last edited on 29 June 2021, at 11:45
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.