- Design and development
- Specifications
- References
name = Polecat | image = LM Polecat.jpg | caption = A picture of the Lockheed-Martin Polecat released at the Farnborough Airshow in 2006 }}{{Infobox Aircraft Type | type = Unmanned aerial vehicle | manufacturer = Lockheed Martin Skunk Works | designer = | first flight = 2005 | introduction = | retired = December 18, 2006 | status = | primary user = | more users = | produced = | number built = 1 | unit cost = | 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. "Polecat" is a colloquialism for a skunk, in an apparent reference to the popular "Skunk Works" nickname for the Lockheed Martin's Advanced Development Programs division. Design and developmentDesignated 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] Specifications{{Aircraft specs |ref= |prime units?=kts |genhide= |crew=0 |capacity={{convert|1000|lb|abbr=on}} of weapons or sensors |length m= |length ft= |length in= |length note= |span m=27.44 |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb=9,000 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=2 |eng1 name=Williams FJ44-3E |eng1 type=turbofan engines |eng1 kw= |eng1 hp= |eng1 shp= |eng1 kn=13.38 |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 shp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 shp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note= |rot number= |rot dia m= |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh= |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance=4 hours |ceiling m= |ceiling ft=65,000 |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |thrust/weight= |more performance=
|armament=
|guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |avionics= }}References1. ^"Farnborough picture: Lockheed Martin Skunk Works releases picture of secret Polecat UAV." Flight International. July 19, 2006. Retrieved July 12, 2013 2. ^"Aviation Week ShowNews Farnborough Day 4 E-zine." Aviation Week & Space Technology. July 20, 2006. 3. ^Butler, A. "Lockheed Unveils Secret Polecat UAV Design." Aviation Week & Space Technology. July 19, 2006.{{dead link |date=January 2017}} 4. ^Trimble, S. "[https://web.archive.org/web/20120118144853/http://www.flightglobal.com/blogs/the-dewline/2007/03/what-killed-the-polecat.html What Killed the Polecat?]." Flightglobal.com. July, 2007.
{{Lockheed aircraft}} 6 : Lockheed Martin aircraft|United States experimental aircraft 2000–2009|Unmanned military aircraft of the United States|Twinjets|Flying wings|Stealth aircraft |