Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

LTV XQM-93

From Wikipedia, the free encyclopedia
Type of aircraft
XQM-93
General information
TypeCommunications relay drone
National originUnited States
ManufacturerLing-Temco-Vought
History
First flightFebruary 1970
Developed fromLTV L450F

TheLing-Temco-Vought XQM-93 is aremotely piloted aircraft developed in the United States in the late 1960s and early 1970s for use as acommunications relay in the Vietnam War. A prototype flew in 1970, but the program was abandoned without producing a service-ready aircraft.

Design and development

[edit]

In the late 1960s, following the early microwave HALE (High Altitude Long Endurance) vehicle studies, theUS Air Force worked withLTV Electrosystems (laterE-Systems) under theCompass Dwell program to build an unmanned aerial vehicle (UAV) using much more conventional turboprop propulsion. At least part of the motivation or inspiration for this effort was derived from theIgloo White program, which was a multiservice attempt to cut the flow of supplies from North Vietnam to South Vietnam through the network of paths and roads running through Cambodia and Laos known as the "Ho Chi Minh Trail".

Igloo White involved seeding the region with thousands of seismic and acoustic sensors, most of them air-dropped, which would pick up indications of traffic along the trail and report them back to a central command center in Thailand, which would dispatch air strikes in response. The sensors were battery-operated and had limited range, so airborne radio relay aircraft orbited above the battle area to pick up the signals and pass them on to the command center.

Originally, the radio relays wereLockheed EC-121 Warning Star aircraft, a military variant of theLockheed L-1049 Super Constellation four piston engined aircraft, but these machines were expensive to operate. They were replaced byBeech Debonaire single-engine light aircraft, modified for the radio relay role and given the military designation of QU-22A. They could be operated as drones, but apparently nobody trusted that as operational practice, and they were never flown unpiloted except as experiments.

LTV Electrosystems' development effort focused on an endurance aircraft that could be flown as a piloted aircraft or a UAV. A number of prototypes, including piloted and UAV versions, were built and flown. They were based on aSchweizer SGS 2-32 sailplane design with major modifications bySchweizer to accommodate aPratt & Whitney Canada PT6A-34 turboprop engine, large fuel tanks, and operational payloads. The aircraft had fixed tricycle landing gear.

The first prototype, designated theL-450F, was piloted. It first flew in February 1970, but was lost in an accident on its third flight in March 1970, the pilot bailing out safely. A second L-450F was built and used to complete the flight test program. The third prototype, the first UAV variant, was designated theXQM-93 and flew in early 1972. It had no cockpit or other provisions for piloted flight. It could carry a payload of 320 kilograms (700 pounds). The Air Force ordered four XQM-93s but it is unclear if they were actually delivered, since Compass Dwell was cancelled that year.

Surviving airframes

[edit]
An LTV XQM-93A on display at theFrontiers of Flight Museum

N2450F cn 002 is now on display in theVintage Flying Museum at Fort Worth Meacham International Airport.[1]

72-1287 is now on display in theFrontiers of Flight Museum at Dallas Love Field Airport.[2]

Specifications (prototype)

[edit]

Data fromJane's All the World's Aircraft 1973–74[3][4]

General characteristics

  • Length: 29 ft 7 in (9.02 m)
  • Wingspan: 57 ft 0 in (17.37 m)
  • Height: 10 ft 8 in (3.25 m)
  • Empty weight: 2,400 lb (1,089 kg)
  • Gross weight: 5,300 lb (2,404 kg)
  • Powerplant: 1 ×Pratt & Whitney PT6A-34 turboprop engine , 475 hp (354 kW)

Performance

  • Cruise speed: 105 mph (170 km/h, 91 kn)
  • Stall speed: 70 mph (114 km/h, 61 kn)
  • Endurance: 24 hours
  • Service ceiling: 50,000 ft (15,240 m)
  • Maximum glide ratio: 28
  • Rate of climb: 914 ft/min (4.6 m/s)

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

[edit]

Notes

[edit]
  1. ^Picture of the E-Systems XQM-93A (L-450F) aircraftArchived 2015-05-09 at theWayback Machine Retrieved 21 May 2013.
  2. ^Ling-Temco-Vought L-450F, 72-1287 / 201287, Frontiers of Flight Museum Retrieved 21 May 2013.
  3. ^Taylor 1973, p. 521
  4. ^Robinson, Anthony (1979).The Illustrated encyclopedia of aviation. Vol. 8. London:Marshall Cavendish. p. 854.ISBN 978-0856855818.

This article contains material that originally came from the web articleUnmanned Aerial Vehicles by Greg Goebel, which exists in the Public Domain.

Bibliography

[edit]
  • Taylor, John W.R., ed. (1973).Jane's All the World's Aircraft 1973–74. London, United Kingdom: Jane's Yearbooks.ISBN 978-0-354-00117-5.

External links

[edit]
Wikimedia Commons has media related toLTV XQM-93.
Manufacturer
designations
By role
Fighters
Scout / Attack
Experimental
Unbuilt
Other
By name
Corsair
Others
1–50
51–100
101–150
151–200
201–
Undesignated
Retrieved from "https://en.wikipedia.org/w/index.php?title=LTV_XQM-93&oldid=1323137236"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp