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McDonnell Douglas F-4 Phantom II

2,640 BlueWhiskySP  8.7 years ago
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The McDonnell Douglas F-4 Phantom II 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. 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.

PERSONAL NOTE: this flies very well for my liking (smooth flight). it turns quickly but doesnt go supersonic. slow speeds (under 190mph) is basically landing/takeoff speed as it tends to flip on its own.
also thanks for 1,600 points, id say it was this time 1 month ago i was at 600, no need to rate because of it, only for the plane

General Characteristics

  • Created On Windows
  • Wingspan 31.3ft (9.5m)
  • Length 43.8ft (13.3m)
  • Height 10.8ft (3.3m)
  • Empty Weight 6,051lbs (2,744kg)
  • Loaded Weight 11,389lbs (5,166kg)

Performance

  • Power/Weight Ratio 1.973
  • Wing Loading 38.9lbs/ft2 (190.0kg/m2)
  • Wing Area 292.7ft2 (27.2m2)
  • Drag Points 2379

Parts

  • Number of Parts 34
  • Control Surfaces 7
  • Performance Cost 198