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Lockheed MQM-105 Aquila

Military Aircraft

The Lockheed MQM-105 Aquila, the name meaning Eagle, was the first small battlefield drone developed in the United States, in the 1970s, to act as a target designator for the US Army. It grew out of a DARPA remotely piloted observation program begun in 1972, and Lockheed was the low bidder when the Army sought a demonstrator in 1975. In 1979 the Lockheed Missile and Space Division won the full-scale development contract for 22 air vehicles. The result was a stealthy tailless aircraft with a pusher propeller driven by a two-stroke piston engine, launched by a truck-mounted hydraulic catapult and recovered by flying into a vertical net. Testing found reliability problems and the aircraft missed 21 of 149 performance specifications at first, and the Department of Defense review board cancelled the program in 1987, although the Army had asked for production.

Facts
Year
1983 1
Engine Class
Piston 1
Status
Cancelled 1
Top Speed (km/h)
210 1
Maximum Mass (kg)
150 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Lockheed MQM-105 Aquila (Wikipedia)

Of Make

Source Lockheed MQM-105 Aquila (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Lockheed MQM-105 Aquila (Wikipedia)Early history, manufacturer
Quote, Early history, manufacturer
Lockheed Missile and Space Division won the contract in late 1979

Originated In

Also in Geography Atlas: where this subject originated.

Source Lockheed MQM-105 Aquila (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
developed in the United States during the 1970s
Sources
1. Lockheed MQM-105 Aquila (Wikipedia)
  • Lead
    was the first small battlefield drone developed in the United States during the 1970s to act as a target designator for the US Army
  • Specifications (Tactical)
    Powerplant: 1 × Virgo M15 two-stroke piston engine , 24 hp (18 kW)
  • Early history
    the DOD review board cancelled the program in 1987
  • Early history, year
    The complete MQM-105 began its contractor flight testing in December 1983
  • Specifications (Tactical), maximum mass
    Gross weight: 263.2 lb (150 kg)
  • Specifications (Tactical), top speed
    Maximum speed: 130 mph (210 km/h, 110 kn)
  • Early history, manufacturer
    Lockheed Missile and Space Division won the contract in late 1979
  • Lead, country of origin
    developed in the United States during the 1970s
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