SPECIFICATIONS
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Wingspan:
13.97m, length:16.70m, height: 4.82m,,
empty mass: 9,595kg,
start mass: 15,700kg, engine1X Khatchaturov R-35-300 afterburning turbojet, 83.6 kN dry, 127 kN afterburning Performance , max speed: 1,350km/h Time to altitudeb: 240m/s, ceiling: 18,500m, range w/max.fuel: 1,150km, armmet: 1x Gryazev-Shipunov GSh-23L 23 mm cannon, Two fuselage, two wing glove, and two wing pylons for up to 3,000 kg (6,610 lb) of stores Crew: 1 |
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status 100%, 2/8/' 07 |
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| Mikojan/Gurevich MiG-23:Fighter 1967 |
U.S.S.R.
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The
The Mikoyan-Gurevich MiG-23 reporting name: "Flogger") is a
swing-wing fighter aircraft, designed by the Mikoyan-Gurevich
bureau in the Soviet Union. It was the first Soviet fighter
with a look-down/shoot-down radar and beyond visual range missiles.
Production started in 1970 and reached large numbers with over
5,000 aircraft built. Today the MiG-23 remains in limited service
with various export customers.
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ソビエトの可変翼戦闘機です。MiG21の後継機として開発されました。しかし主翼が可変翼で兵装の搭載個所(パイロン)が少なく満足できる性能ではありませんでした。しかし前線での作戦を主眼としていたので戦闘爆撃機の能力もあり共産圏で広く使用されました。またアビオニクスなどを簡素化して戦闘爆撃機に特化したMiG27も開発されています。
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