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The McDonnell Douglas F-4 Phantom II [N 1] is an American tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber that was developed by McDonnell Aircraft for the United States Navy. [3]
Max speed at low altitude 1480 km/h. Crew: 2. Unique in that it was used by US Air Force, US Navy and US Marine. British version used Rolls Royce Spey engines (F-4K, F-4N). Some Phantom versions were equipped with a Raytheon APG-65 radar with 100 km range. Internal armament M61A1 V (...)
The McDonnell F-4 Phantom II is a twin-engined two-seat jet fighter and fighter bomber aircraft produced by the US-American manufacturer McDonnell Aircraft Corporation, later McDonnell Douglas Corporation. The F-4 Phantom II was also operated from aircraft carriers.
7 lut 2024 · Page details technical specifications, development, and operational history of the McDonnell Douglas F-4 Phantom II Multirole / Carrierbased Fighter / Strike Fighter Aircraft including pictures.
McDonnell Douglas F-4 Phantom II – dwumiejscowy, naddźwiękowy samolot myśliwsko-bombowy dalekiego zasięgu zdolny do działania w każdych warunkach pogodowych.
29 maj 2014 · Specifications F-4 Phantom II F-4E. Powerplant: two 79.62 kN (17,900 lb st) General Electric J79-GE-17A turbojets. Dimensions: length 19.20m (63 ft 0 in); height 5.02m (16 ft 5½ in); wing span 11.77m (38ft 7½ in) Weights: take-off ('clean') 18.818 kg (41,487 lb); Max Take-Off Weight 28.030 kg (61,795 lb)
The two-place, twin-engine, all-weather supersonic F-4 Phantom II flew at Mach 2 (twice the speed of sound), and could carry a payload of up to 16,000 pounds of bombs, rockets, missiles and guns. Each aircraft had 54,197 feet of wiring and 643,000 fasteners holding it together.
