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
Engine Class EngineWestinghouse XJ81-WE-3 turbojet 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Northrop AQM-35 (Wikipedia)
Of Make
Source Northrop AQM-35 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Northrop AQM-35 (Wikipedia)LeadQuote, 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 originQuote, 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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