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Douglas F3D Skyknight
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Douglas F3D Skyknight : ウィキペディア英語版
Douglas F3D Skyknight


The Douglas F3D Skyknight (later designated F-10 Skyknight) was a United States twin-engined, mid-wing jet fighter aircraft manufactured by the Douglas Aircraft Company in El Segundo, California. The F3D was designed as a carrier-based all-weather night fighter and saw service with the United States Navy and United States Marine Corps. The mission of the F3D was to search out and destroy enemy aircraft at night.〔''Standard Aircraft Characteristics F3D-2 Skyknight'' NAVAER 1335C REV. 10-51.〕
The F3D Skyknight was never produced in great numbers but it did achieve many firsts in its role as a night fighter over Korea. While it never achieved the fame of the North American F-86 Sabre, it did down several Soviet-built MiG-15s as a night fighter over Korea with only one air-to-air loss of its own against a Chinese MiG-15, which occurred on the night of 29 May 1953.〔("Defense POW/Missing Personnel Office: Korean War Air Loss Database (KORWALD)." ) ''dtic.mil.'' Retrieved: 10 August 2013.〕〔Zhang 2002, pp. 194–195.〕
The Skyknight played an important role in the development of the radar-guided AIM-7 Sparrow missile which led to further guided air-to-air missile developments. It also served as an electronic warfare platform in the Vietnam War as a precursor to the EA-6A Intruder and EA-6B Prowler. The aircraft is sometimes unofficially called "Skynight", dropping the second "k". The unusual, portly profile earned it the nickname "Willie the Whale".〔("Douglas Skyknight." ) ''Boeing history.'' Retrieved: 23 August 2010.〕 Some Vietnam War U.S. Marine veterans have referred to the Skyknight as "Drut", whose meaning becomes obvious when read backwards. This may be in reference to its age, unflattering looks or its low-slung air intakes that made it vulnerable to foreign object damage (FOD).〔
==Design and development==
The F3D was not intended to be a typical sleek and nimble dogfighter, but as a standoff night fighter, packing a powerful radar system and a second crew member. It originated in 1945 with a US Navy requirement for a jet-powered, radar-equipped, carrier-based night fighter. The Douglas team led by Ed Heinemann designed around the bulky air intercept radar systems of the time, with side-by-side seating for the pilot and radar operator.〔Donald 1997, p. 365.〕 The result was an aircraft with a wide, deep, and roomy fuselage. Instead of ejection seats, an escape tunnel was used, similar to the type used in the A-3 Skywarrior.〔
The XF3D-1 beat out Grumman Aircraft Engineering Corporation's G-75 two-seat, four-engined, Westinghouse J30-powered night fighter design, and a contract was issued on 3 April 1946. The US Navy's Bureau of Aeronautics (BuAer) also issued a contract to Grumman for two G-75 (company designation) XF9F-1 (BuAer designation) experimental aircraft on 11 April 1946 in case the Skyknight ran into problems. Grumman soon realized that the G-75 was a losing design but had been working on a completely different, single-engined day fighter known as the Grumman G-79 which became the F9F Panther.〔Sullivan 1982, pp. 4, 6.〕
The first flight of the XF3D-1 was on 23 March 1948 at Douglas' El Segundo facility with test pilot Russell Thaw at the controls. Further flight testing followed at El Segundo until October 1948. Three prototypes were then taken to Muroc Air Force Base (later renamed Edwards Air Force Base) for service trials. These units were powered by two Westinghouse J34-WE-24 turbojets of 3,000 lbf (1,361 kgf) thrust, mounted under the roots of then-standard straight wings of the early jet era. A production contract for 28 F3D-1 J34-WE-32 powered production aircraft was issued in June 1948 with the first production aircraft flying on 13 February 1950.〔Gunston 1981, p. 172.〕
As a night fighter that was not expected to be as fast as smaller daylight fighters, the expectation was to have a stable platform for its radar system and the four 20 mm cannon mounted in the lower fuselage. The F3D was, however, able to outturn a MiG-15.〔Dorr 1994, p. 154.〕 The fire control system in the F3D-1 was the Westinghouse AN/APQ-35. The AN/APQ-35 was advanced for the time, a combination of three different radars, each performing separate functions: an AN/APS-21 search radar, an AN/APG-26 tracking radar, both located in the nose, and an AN/APS-28 tail warning radar.〔Badrocke 1993, pp. 41, 44–45.〕 The complexity of this vacuum tube-based radar system, which was produced before the advent of semiconductor electronics, required intensive maintenance to keep it operating properly.
The F3D-1 was followed by the F3D-2, which was first ordered in August 1949. The F3D-2 was intended to have Westinghouse J46 engines in enlarged nacelles to replace the J34-WE-32 engines of the F3D-1, but because of development problems with the J46, the F3D-2 was initially fitted with J34-WE-36 engines instead. Higher-thrust J34-WE-38 engines which increased aircraft performance were installed later.〔 The F3D-2 also incorporated an improved Westinghouse AN/APQ-36 fire control system. A total of 237 F3D-2s were built before production ended on 23 March 1952. A higher performance F3D-3 version with swept wings and J46 engines was planned, but was cancelled when the trouble-plagued J46 engine program was terminated.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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