- Specifications
- References
- External links
{{more citations needed|date=November 2010}} name= AQM-60 Kingfisher | image=Aqm-60a.jpg | caption=AQM-60 Kingfisher awaiting loading onto its B-50 mothership before a test of US air defenses. }}{{Infobox aircraft type | type= Target drone | national origin=United States of America | manufacturer=Lockheed | designer= | first flight=April 1951 | introduced= | retired= | status= | primary user= United States Air Force | more users= | produced= | number built= | program cost= | unit cost= | developed from=Lockheed X-7 | variants with their own articles= | developed into= }} |
The AQM-60 Kingfisher, originally designated XQ-5, was a target drone version of the USAF's X-7 test aircraft built by the Lockheed Corporation. The aircraft was designed by Kelly Johnson, the designer who later went on to create the Lockheed SR-71 Blackbird and its relatives, such as the Lockheed A-12 and Lockheed YF-12.{{sfn|National Aviation Hall of Fame}} The X-7's development began in 1946 after a request from the USAF for a Mach 3 unmanned aerial vehicle for test purposes. This unmanned test craft eventually evolved into the Kingfisher, which was later used to test anti-missile systems such as the MIM-3 Nike Ajax, SAM-A-25/MIM-14 Nike Hercules, and IM-99/CIM-10.[1] The Kingfisher was capable of evading the vast majority of weapons systems it was used to test, despite the systems being designed to destroy hypersonic missiles in flight. This created a significant amount of embarrassment at the USAF, resulting in considerable political fallout, which led to the eventual discontinuation of production in 1959 and the cancellation of the project entirely in the mid-1960s.[2] The engine developed for the AQM-60 was later modified for use on a long range nuclear tipped ramjet called the CIM-10 Bomarc, which was used as a nationwide defense against nuclear bombers during the 1960s and early 1970s. An endurance variant of the same engine was produced in order to be used in the Lockheed D-21, which was designed to be launched off the back of a Lockheed SR-71 Blackbird mothership or from under the wing of a Boeing B-52 Stratofortress nuclear bomber.[3] Specifications {{Aircraft specs |ref= |prime units?=kts |genhide= |crew= |capacity= |length m=11.6 |length ft= |length in= |length note= |span m=3 |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=20 |dia note= |width m= |width ft= |width in= |width note= |height m=2.1 |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=3,600 |gross weight lb= |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=1 |eng1 name=Marquardt XRJ43-MA |eng1 type=ramjet |eng1 kw= |eng1 hp= |eng1 shp= |eng1 kn= |eng1 lbf= |eng1 note=(Sustainer) |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number=2 |eng2 name=Thiokol XM45 (5KS50000) |eng2 type=solid-fuel rockets |eng2 kw= |eng2 hp= |eng2 shp= |eng2 kn=222 |eng2 lbf= |eng2 note= for 5s (Boosters) |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=4.3 |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=210 |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= |ceiling m=30,000 |ceiling ft= |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= }} References 1. ^Area 51 - Black Jets: A History of the Aircraft Developed at Groom Lake, Bill Yenne 2014, p.95 2. ^{{cite web|url=http://www.456fis.org/LOCKHEED_X-7.htm|title=The Lockheed X-7|author=|date=|website=www.456fis.org|accessdate=12 April 2018}} 3. ^Goodall and Goodall 2002, p. 106.
- {{cite web|url=http://www.nationalaviation.org/johnson-clarence-leonard/|title=Johnson, Clarence Leonard - National Aviation Hall of Fame|website=nationalaviation.org|accessdate=12 April 2018|ref={{harvid|National Aviation Hall of Fame}} }}
External links{{commons category|Lockheed X-7}}- Directory of US Military Rockets and Missiles
- http://www.designation-systems.net/dusrm/m-60.html
{{Lockheed aircraft}}{{US missiles}}{{USAF drones}} 7 : Lockheed aircraft|United States special-purpose aircraft 1950–1959|Target drones of the United States|Single-engined jet aircraft|Ramjet-powered aircraft|Aircraft with auxiliary rocket engines|Mid-wing aircraft |