McDONNELL F-4 PHANTOM II

 

ORIGIN:

United States of America

DESCRIPTION:

Two-seat tactical strike fighter

POWER PLANT:

(F-4E)

Two 11,870 lb dry and 17,900 lb st with reheat General Electric J79-GE-17 turbojets

SPECIFICATIONS:

  • Wingspan: 11.7 m (38 ft 4¾ in)
  • Length: 19.20 m (62 ft 10½ in)
  • Height: 4.96 m (16 ft 3½ in)
  • Wing area: 49.2 m² (530 sq ft)
  • Max speed (clean): 2,304 km/h (1,432 mph)
  • Max speed with external stores: 1,464 km/h (910 mph)
  • Service ceiling: 18,975 m (62,250 ft)
  • Initial rate of climb (clean): 15,180 m/min (49,800 ft/min)
  • Operating radius with four AIM-7F Sparrow air-to-air missiles and two fuel tanks on hi-lo-hi mission: 680 km (422 miles)
  • Ferry range 2,593 km (1,611 miles) at 925 km/h (575 mph) at: 12,190 m (40,000 ft)
  • Empty weight: 13,801 kg (30,425 lb)
  • Loaded weight with four Sidewinder missiles and max external fuel: 26,308 kg (58,000 lb)
  • Max overloaded weight: 27,502 kg (60,630 lb)

PHOTO SOURCE:

F-4 Phantom II, Davis-Monthan - McDonnell Douglas F-4 Phantom II – Wikipedia, wolna encyklopedia

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