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Mcdonnel Douglas F-4 Phantom II

10.4k RandyAndSonsAircraft  7.8 years ago

Action group 1 for dropping tanks , airbrakes and steering of wheels exist. The McDonnell Douglas F-4 Phantom II[N 1] is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor aircraft/fighter-bomber originally developed for the United States Navy by McDonnell Aircraft.[1] It first entered service in 1960 with the U.S. Navy. Proving highly adaptable, it was also adopted by the U.S. Marine Corps and the U.S. Air Force, and by the mid-1960s had become a major part of their respective air wings.[2] The Phantom is a large fighter with a top speed of over Mach 2.2. It can carry more than 18,000 pounds (8,400 kg) of weapons on nine external hardpoints, including air-to-air missiles, air-to-ground missiles, and various bombs. The F-4, like other interceptors of its time, was designed without an internal cannon. Later models incorporated an M61 Vulcan rotary cannon. Beginning in 1959, it set 15 world records for in-flight performance,[3] including an absolute speed record, and an absolute altitude record.[4]

General Characteristics

  • Created On Windows
  • Wingspan 42.7ft (13.0m)
  • Length 42.6ft (13.0m)
  • Height 13.4ft (4.1m)
  • Empty Weight 12,132lbs (5,503kg)
  • Loaded Weight 20,722lbs (9,399kg)

Performance

  • Power/Weight Ratio 3.253
  • Wing Loading 57.8lbs/ft2 (282.0kg/m2)
  • Wing Area 358.7ft2 (33.3m2)
  • Drag Points 3800

Parts

  • Number of Parts 77
  • Control Surfaces 7
  • Performance Cost 502