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LTV L450F

From Wikipedia, the free encyclopedia
L450F
RoleReconnaissance aircraft
Type of aircraft
ManufacturerLing-Temco-Vought
First flightFebruary 1970
Primary userUnited States Air Force
Developed fromSchweizer SGS 2-32
Developed intoLTV XQM-93

TheLTV L450F, also known as theL45ØF,[1] was a prototype quietreconnaissance aircraft, developed byLing-Temco-Vought in the late 1960s for use in theVietnam War by theUnited States. Based on the airframe of aSchweizer 2-32 sailplane, the aircraft flew in 1970, and was developed into theXQM-93 reconnaissancedrone before the project was cancelled.

Design and development

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Developed as a follow on to theIgloo White program, the L450F was intended to provide a quiet reconnaissance and communications relay aircraft.[1] Under a $1 millionUSD contract by LTV Electrosystems, the L450F was developed from aSchweizer SGS 2-32sailplane, modified by Schweizer to LTV's specifications.[1]

These modifications included stronger wingspars, thicker wing skin, installation of aPratt & Whitney PT6A turboprop engine driving a three-bladed propeller, and main landing gear based on that of theGrumman Ag-Cat agricultural aircraft.[1] An alternative configuration, using apiston engine, was also proposed.[1]

The prototype L450F first flew in February 1970, but was destroyed during its third flight, on 23 March that year, the pilot successfully bailing out. A second prototype was then completed and flown, successfully completing the testing program, and a third prototype was ordered as the unmannedXQM-93 drone, under theCompass Dwell project. Four examples of the XQM-93 were contracted for by theUnited States Air Force, however the Compass Dwell project was subsequently cancelled.[1][2]

Operational history

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The second L450F on display

27 March 1972 Donald R. Wilson reached the altitude of 15,456 m (50,708 ft) in horizontal flight flying the remaining L450F,registered N2450F, setting a newFédération Aéronautique Internationale international record, Class C-1c, Group II[3] (Powered aeroplanes, takeoff weight 1000 to 1750 kg, turboprop). This record still stood as of 27 March 2012.

Specifications (prototype)

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Data from Janes[1]

General characteristics

  • Crew: 1 (pilot)
  • Length: 29 ft (8.8 m)
  • Wingspan: 57 ft (17 m)
  • Empty weight: 2,400 lb (1,089 kg)
  • Max takeoff weight: 4,600 lb (2,087 kg)
  • Fuel capacity: 2,300 pounds (1,000 kg)
  • Powerplant: 1 ×Pratt & Whitney PT6A-29 , 778 shp (580 kW)
  • Propellers: 3-bladedHartzell

Performance

  • Cruise speed: 105 mph (169 km/h, 91 kn)
  • Range: 6,000 mi (9,650 km, 5,210 nmi)
  • Endurance: 24–30 hours
  • Service ceiling: 52,000 ft (16,000 m)
  • Maximum glide ratio: 28:1
  • Rate of climb: 2,600 ft/min (13 m/s)

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

References

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Notes

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  1. ^abcdefgJane's 1971, p. 344-345
  2. ^Goebel, Greg."The Prehistory of Endurance UAVs"[usurped].VectorSite. Accessed 18 June 2010.
  3. ^"Fai Record File". Fai.org. Retrieved5 May 2012.

Bibliography

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  • Taylor, John W.R. (ed.)Jane's All The World's Aircraft 1971–1972. London: Sampson Low Marston & Co, 1971.ISBN 0 354-000-942.

External links

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Media related toLTV L450F at Wikimedia Commons

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