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Published byStanley Mason Modified over 9 years ago
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Corp. Vilém Marek
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Replaced F-4 Phantom II Designed as an air superiority fighter and a long- range naval interceptor First fly in 1970 First deployment in 1974 Replaced by F/A-18 Super Hornet in 2006
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Crew: 2 (Pilot and Radar Intercept Officer) Length: 62 ft 9 in (19.1 m) Wingspan: Spread: 64 ft (19.55 m) Swept: 38 ft (11.58 m) Height: 16 ft (4.88 m) Wing area: 565 ft² (54.5 m²) Empty weight: 43,735 lb (19,838 kg) Loaded weight: 61,000 lb (27,700 kg) Maximum speed: Mach 2.34 (1,544 mph, 2,485 km/h) at high altitude Rate of climb: >45,000 ft/min (229 m/s)
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For high-speed intercept, they are swept back and they swing forward for lower speed flight. 20° - 68° in flight Up to 75° for parking Automatically controlled by computer Pilots can manually override the system
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F-14A - 1970 F-14B - 1987 F-14D - 1991 Differences in engines and avionics
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Can carry over 6,700 kg (14,800 lb) 20 mm M61 Vulcan Gatling cannon Missiles: AIM-54 Phoenix AIM-7 Sparrow AIM-9 Sidewinder
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documentary http://www.youtube.com/watch?v=4arJFZbfKAg promo http://www.youtube.com/watch?v=Y45rzmDaABI
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