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Northrop AQM-35

Military Aircraft

The Northrop AQM-35, first known as the Q-4, was an American supersonic target drone built by the Northrop Corporation for the United States Air Force. The programme began in 1953 as the Radioplane RP-61, and in June 1954 the Air Force contracted Northrop to develop it; the first flight-capable XQ-4 was launched in 1956. It was powered by a Westinghouse XJ81-WE-3 turbojet that took it to Mach 1.55, could be ground or air launched from a Lockheed DC-130 Hercules drone controller, followed by radar and commanded by radio telemetry, and came down on a three-stage parachute system cushioned by four inflatable airbags. It served as a target for surface-to-air and air-to-air missiles, with a secondary reconnaissance role planned. The Q-4B added a General Electric J85 engine and a stronger airframe, and in 1963 the family became the AQM-35A and AQM-35B. The type was never judged a full success, only 25 were built, and the last were retired during the 1960s.

Facts
Year
1956 1
Engine Class
Jet 1
Status
Out of production 1
Units Built
25 1
Mass (kg)
898 1
Engine
Westinghouse XJ81-WE-3 turbojet 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Northrop AQM-35 (Wikipedia)

Of Make

Source Northrop AQM-35 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Northrop AQM-35 (Wikipedia)Lead
Quote, Lead
The AQM-35 was a supersonic target drone produced by the Northrop Corporation.

Originated In

Also in Geography Atlas: where this subject originated.

Source Northrop AQM-35 (Wikipedia)Overview, country of origin
Quote, Overview, country of origin
In June 1954 the United States Air Force awarded Northrop a contract for development of the project as the Q-4
Sources
1. Northrop AQM-35 (Wikipedia)
  • Overview
    the first flight-capable XQ-4 was launched in 1956
  • Lead
    The AQM-35 was a supersonic target drone produced by the Northrop Corporation.
  • Overview, engine class
    It was powered by a Westinghouse XJ81-WE-3 turbojet
  • Overview, total built
    Only 25 of all types were ever built.
  • Overview, retirement
    The last examples of the type were retired during the 1960s.
  • Specifications, Q-4 and AQM-35A empty weight
    Empty weight: 1,980 lb (898 kg)
  • Overview, country of origin
    In June 1954 the United States Air Force awarded Northrop a contract for development of the project as the Q-4
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