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MIG-25 : ウィキペディア英語版
Mikoyan-Gurevich MiG-25

The Mikoyan-Gurevich MiG-25 ((ロシア語:Микоян и Гуревич МиГ-25)) (NATO reporting name: Foxbat) is a supersonic interceptor and reconnaissance aircraft that was among the fastest military aircraft to enter service. It was designed by the Soviet Union's Mikoyan-Gurevich bureau. The first prototype flew in 1964, and the aircraft entered service in 1970. It has an operational top speed of Mach 2.83 (Mach 3.2 is possible but at risk of significant damage to the engines), and features a powerful radar and four air-to-air missiles.
When first seen in reconnaissance photography, the large wing suggested an enormous and highly maneuverable fighter, at a time when U.S. design theories were also evolving towards higher maneuverability due to combat performance in the Vietnam War. The appearance of the MiG-25 sparked serious concern in the West and prompted dramatic increases in performance for the McDonnell Douglas F-15 Eagle then under development in the late 1960s. The capabilities of the MiG-25 were better understood in 1976 when Soviet pilot Viktor Belenko defected in a MiG-25 to the United States via Japan. It turned out that the aircraft's weight necessitated its large wings.
Production of the MiG-25 series ended in 1984 after completion of 1,190 aircraft. A symbol of the Cold War, the MiG-25 flew with Soviet allies and former Soviet republics, remaining in limited service in Russia and several other nations. It is one of the highest-flying military aircraft, and the second fastest after the SR-71 reconnaissance aircraft.〔("Global Aircraft – Top 50 Fastest Aircraft." ) ''The Global Aircraft Organization,'' 24 April 2007. Retrieved: 30 June 2011.〕
==Design and development==


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Mikoyan-Gurevich MiG-25」の詳細全文を読む



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