Profile image

F4 Phanton II

785 SunFireFighters  6.7 years ago
16 downloads
No Tags

---WIKIPEDIA---The McDonnell Douglas F-4 Phantom II[N 1] is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber originally developed for the United States Navy by McDonnell Aircraft.[2] 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 air wings.[3] 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,[4] including an absolute speed record, and an absolute altitude record.[5] The F-4 was used extensively during the Vietnam War. It served as the principal air superiority fighter for both the Navy and Air Force, and became important in the ground-attack and aerial reconnaissance roles late in the war. The Phantom has the distinction of being the last U.S. fighter flown by pilots who attained ace status in the 20th century. During the Vietnam War, one U.S. Air Force pilot and two weapon systems officers (WSOs),[6] and one U.S. Navy pilot and one radar intercept officer (RIO) became aces by achieving five aerial kills against enemy fighter aircraft.[7] The F-4 continued to form a major part of U.S. military air power throughout the 1970s and 1980s, being gradually replaced by more modern aircraft such as the F-15 Eagle and F-16 in the U.S. Air Force, the Grumman F-14 Tomcat in the U.S. Navy, and the F/A-18 Hornet in the U.S. Navy and U.S. Marine Corps. The F-4 Phantom II remained in use by the U.S. in the reconnaissance and Wild Weasel (Suppression of Enemy Air Defenses) roles in the 1991 G

General Characteristics

  • Created On Windows
  • Wingspan 39.9ft (12.2m)
  • Length 47.6ft (14.5m)
  • Height 14.6ft (4.5m)
  • Empty Weight 20,503lbs (9,300kg)
  • Loaded Weight 25,169lbs (11,416kg)

Performance

  • Power/Weight Ratio 2.678
  • Wing Loading 64.6lbs/ft2 (315.6kg/m2)
  • Wing Area 389.4ft2 (36.2m2)
  • Drag Points 5703

Parts

  • Number of Parts 126
  • Control Surfaces 6
  • Performance Cost 643