Fleetwings BQ-2

{{Short description|1940s American unmanned aerial vehicle}}

{{Use American English|date=October 2024}}

{{Use dmy dates|date=October 2024}}

{{Infobox aircraft begin

|name = XBQ-2

|image = Fleetwings XBQ-2A.jpg

|size = 300px

|alt =

|caption =

|long caption =

}}{{Infobox aircraft type

|type = Flying bomb

|national origin = United States

|manufacturer = Fleetwings

|designer =

|design group =

|first flight = 1943

|introduced =

|introdction =

|retired =

|status =

|primary user = United States Army Air Forces

|more users =

|produced =

|number built = 1

|program cost =

|unit cost =

|developed from =

|variants with their own articles = Fleetwings BQ-1

|developed into =

}}

The Fleetwings BQ-2 was an early expendable unmanned aerial vehicle — referred to at the time as an "assault drone" — developed by Fleetwings during the Second World War for use by the United States Army Air Forces. Only a single example of the type was built; the aircraft was deemed too expensive for service and was cancelled after a brief flight testing career.

Development

Development of the BQ-2 began on 10 July 1942, under a program for the development of "aerial torpedoes" – unmanned flying bombs – that had been instigated in March of that year. Fleetwings was contracted to build a single XBQ-2 assault drone,Werrell 1985, p.30. powered by two Lycoming XO-435 horizontally opposed piston engines, and fitted with a fixed landing gear in tricycle configuration; the landing gear was jettisonable for better aerodynamics.

The BQ-2 was optionally piloted; a single-seat cockpit was installed for ferry and training flights; a fairing would replace the cockpit canopy on operational missions.Parsch 2005 The BQ-2 was intended to carry a {{convert|2000|lb}} warhead over a range of {{convert|1717|mi}} at {{convert|225|mph}}; the aircraft would be destroyed in the act of striking the target. A single BQ-1 was to be constructed as well under the same contract.

Flight testing

The XO-435 engines were dropped from the design of the XBQ-2 before completion, being replaced by two Lycoming R-680 radial engines, with the aircraft being redesignated XBQ-2A.Andrade 1979, p.60.

Following trials of the television-based command guidance system using a PQ-12 target drone, the XBQ-2A flew in mid 1943; following flight trials, the design was determined to be too expensive for operational use, and the program was cancelled in December of that year.

Specifications (XBQ-2A)

File:Fleetwings XBQ-2A front.jpg

{{Aircraft specs

|ref=

|prime units?=imp

|crew=1 (optional)

|capacity=

|length m=

|length ft=

|length in=

|length note=

|span m=

|span ft=48

|span in=7

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=

|wing area sqft=

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=

|empty weight note=

|gross weight kg=

|gross weight lb=7700

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=2

|eng1 name=Lycoming R-680-13

|eng1 type=radial piston engines

|eng1 kw=

|eng1 hp=280

|eng1 shp=

|eng1 note=

|power original=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=y

|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=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|more performance=

|armament=* {{convert|2000|lb}} warhead

|guns=

|bombs=

|rockets=

|missiles=

|hardpoints=

|hardpoint capacity=

|hardpoint rockets=

|hardpoint missiles=

|hardpoint bombs=

|hardpoint other=

|avionics=

}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

|similar engines=

}}

References

{{commons category|Fleetwings BQ-2}}

;Notes

{{reflist}}

;Bibliography

{{refbegin}}

  • {{cite book|last=Andrade|first=John|title=U.S. Military Aircraft Designations and Serials since 1909|year=1979|publisher=Midland Counties Publications|location=Leicester, UK|isbn=0-904597-22-9}}
  • {{cite web |url=http://www.designation-systems.net/dusrm/app1/bq-1.html |title= Fleetwings BQ-1/2 |first=Andreas |last=Parsch |year=2005 |work=Directory of U.S. Military Rockets and Missiles, Appendix 1: Early Missiles and Drones |publisher=designation-systems.net |access-date=22 January 2013}}
  • {{cite book|last=Werrell|first=Kenneth P.|title=The Evolution of the Cruise Missile|year=1985|publisher=Air University Press|location=Maxwell AFB, Alabama|isbn=978-1478363057}}

{{refend}}

{{Fleetwings aircraft}}

{{US unmanned aircraft}}

BQ-2

Category:1940s United States bomber aircraft

Category:Unmanned aerial vehicles of the United States

Category:World War II guided missiles of the United States

Category:Cancelled military aircraft projects of the United States

Category:High-wing aircraft

Category:Aircraft first flown in 1943

Category:Twin piston-engined tractor aircraft

Category:Aircraft with fixed tricycle landing gear