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LTV XQM-93

Military Aircraft

The Ling-Temco-Vought XQM-93 was a remotely piloted aircraft developed in the United States in the late 1960s and early 1970s as a communications relay for the Vietnam War. The United States Air Force worked with LTV Electrosystems under the Compass Dwell program to build a drone with ordinary turboprop propulsion, inspired in part by the Igloo White program, whose ground sensors along the Ho Chi Minh Trail needed airborne radio relays. The airframe was based on a Schweizer SGS 2-32 sailplane, heavily modified by Schweizer to take a Pratt & Whitney Canada PT6A-34 turboprop, large fuel tanks and payloads of up to 320 kilograms, with fixed tricycle landing gear. It followed the piloted L450F and flew in early 1972 without cockpit or provision for a pilot. The Air Force ordered four, but Compass Dwell was cancelled that year and the program produced no service-ready aircraft. Two airframes survive in museums in Texas.

Facts
Year
1972 1
Engine Class
Turboprop 1
Status
Cancelled 1
Power (kW)
354 1
Mass (kg)
1089 1
Maximum Mass (kg)
2404 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source LTV XQM-93 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source LTV XQM-93 (Wikipedia)Lead
Quote, Lead
The Ling-Temco-Vought XQM-93 is a remotely piloted aircraft developed in the United States in the late 1960s and early 1970s for use as a communications relay in the Vietnam War.

Originated In

Also in Geography Atlas: where this subject originated.

Source LTV XQM-93 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
developed in the United States in the late 1960s and early 1970s
Sources
1. LTV XQM-93 (Wikipedia)
  • Lead
    The Ling-Temco-Vought XQM-93 is a remotely piloted aircraft developed in the United States in the late 1960s and early 1970s for use as a communications relay in the Vietnam War.
  • Lead, status
    A prototype flew in 1970, but the program was abandoned without producing a service-ready aircraft.
  • Design and development
    The third prototype, the first UAV variant, was designated the XQM-93 and flew in early 1972.
  • Design and development, engine
    accommodate a Pratt & Whitney Canada PT6A-34 turboprop engine, large fuel tanks, and operational payloads.
  • Specifications
    Powerplant: 1 × Pratt & Whitney PT6A-34 turboprop engine , 475 hp (354 kW)
  • Specifications, mass
    Empty weight: 2,400 lb (1,089 kg)
  • Specifications, maximum mass
    Gross weight: 5,300 lb (2,404 kg)
  • Lead, country of origin
    developed in the United States in the late 1960s and early 1970s
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