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Simplistic F-4E Phantom II

74.9k L1nus  1.3 years ago

The McDonnell Douglas F-4 Phantom II is an American tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber originally developed by McDonnell Aircraft for the United States Navy

Ag-1 for arresting hook
Ag-2 for Afterburner (activates when 100% throttle is applied)
Ag-3 to jettison ordnance
Ag-4 to use taxi motor (pitch for forward and reverse)
Ag-5 for emergency parachute

Trim down for flaps
Vtol up for airbrakes


General Characteristics

  • Successors 1 airplane(s) +84 bonus
  • Created On Windows
  • Wingspan 30.6ft (9.3m)
  • Length 49.7ft (15.1m)
  • Height 12.7ft (3.9m)
  • Empty Weight N/A
  • Loaded Weight 7,869lbs (3,569kg)


  • Power/Weight Ratio 2.484
  • Wing Loading 37.1lbs/ft2 (181.3kg/m2)
  • Wing Area 211.9ft2 (19.7m2)
  • Drag Points 244


  • Number of Parts 325
  • Control Surfaces 7
  • Performance Cost 1,396