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[[Category:United States special-purpose aircraft 1955-1959]] |
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[[Category:UAVs and drones]] |
[[Category:UAVs and drones]] |
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[[Category:Unmanned vehicles]] |
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[[Category:Modern missiles of the United States]] |
[[Category:Modern missiles of the United States]] |
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The AQM-35 was a supersonic target drone produced by Northrop.
The AQM-35 program began life in 1953 as the Model RP-61 supersonic target drone. In June 1954 the United States Air Force awarded Northrop a contract for development of the project as the Q-4; the first flight-capable XQ-4 was launched in 1956.
The XQ-4 was capable of either ground or air launch, though the former mode was never tested. It was powered by an XJ81-WE-3 turbojet, allowing it to reach speeds of Mach 1.55. The drone's course was followed with radar, and flight commands were sent by a radio telemetry system. When the mission was completed the XQ-4 would deploy a three-stage parachute system along with four large inflatable airbags to cushion the impact with the ground.
The Air Force planned to use the Q-4 as a target for various surface-to-air and air-to-air missiles. A secondary reconnaissance function was planned, with TV or cameras carried. The drone was air-launched by a Lockheed DC-130 Hercules drone controller aircraft, or other carrier aircraft.
In1963, the Q-4 family of drones were given the designation AQM-35A and AQM-35B. They were never considered entirely successful, with a variety of problems arising during both the development and flight testing phases. It was also considered that the flight performance of the drone was so high that it was not a realistic test for the missiles being developed - ironic since the whole point of the project was to develop a supersonic target. Only 25 of all types were ever built. The last examples of the type were retired during the 1960s.
The XQ-4A, was developed to use a have a Fairchild J83 engine and a modified radar signature for testing the CIM-10 Bomarc missile. When the engine could not be developed in time the variant was cancelled.
In1959 Northrop was given a contract to develop an improved XQ-4B fitted with a much more powerful J85-GE-5 engine and a strengthened airframe. This variant was first flown in 1961.
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General characteristics
Performance
General characteristics
Performance
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