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Douglas F-4 Phantom II "1958"

The Douglas A-1 Skyraider (formerly known as AD Skyraider) is an American single-seat attack aircraft that saw service between the late 1940s and early 1980s. The Skyraider had a remarkably long and successful career; it became a piston-powered, propeller-driven anachronism in the jet age, and was nicknamed "Spad", after the French World War I fighter

Douglas: F-4E Phantom II

Role Interceptor, fighter-bomber
National origin United States
Manufacturer McDonnell Aircraft Corporation
McDonnell Douglas
First flight 27 May 1958
Introduction 1961
Retired 1992 (United Kingdom) 1996 (U.S. combat use)
Status In limited service
Primary users United States Air Force (historical)
United States Navy (historical) / United States Marine Corps 
Produced 1958–1981
Number built 5,195
Variants McDonnell Douglas Phantom FG.1/FGR.2


Douglas Aircraft

The McDonnell Douglas F-4 Phantom II is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber

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Douglas
F-4E Phantom "1958

The McDonnell Douglas F-4 Phantom II is a 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.[2] Proving highly adaptable, it first entered service with the Navy in 1961[3] before it was adopted by the United States Marine Corps and the United States Air Force, and by the mid-1960s it had become a major part of their air arms.[4] Phantom production ran from 1958 to 1981 with a total of 5,195 aircraft built, making it the most produced American supersonic military aircraft in history, and cementing its position as an iconic combat aircraft of the Cold War.[

Design

 

Unlike the U.S. Navy and U.S. Marine Corps, which flew the Phantom with a Naval Aviator (pilot) in the front seat and a Naval Flight Officer as a radar intercept officer (RIO) in the back seat, the USAF initially flew its Phantoms with a rated Air Force Pilot in front and back seats. Pilots usually did not like flying in the back seat;[19] while the GIB, or “guy in back”, could fly and ostensibly land the aircraft, he had fewer flight instruments and a very restricted forward view. The Air Force later assigned a rated Air Force Navigator qualified as a weapon/targeting systems officer (later designated as weapon systems officer or WSO) in the rear seat instead of another pilot

Operators

Operators

 Greece
 Iran
 South Korea
 Turkey

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Douglas F-4E Phantom II (1958)

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 Gulf War, finally leaving service in 1996.[10][11] It was also the only aircraft used by both U.S. flight demonstration teams: the United States Air Force Thunderbirds (F-4E) and the United States Navy Blue Angels (F-4J).[4][12][13] The F-4 was also operated by the armed forces of 11 other nations. Israeli Phantoms saw extensive combat in several Arab–Israeli conflicts, while Iran used its large fleet of Phantoms, acquired before the fall of the Shah, in the Iran–Iraq War.

Specifications

General characteristics

  • Crew: 2
  • Length: 63 ft 0 in (19.2 m)
  • Wingspan: 38 ft 5 in (11.7 m)
  • Height: 16 ft 5 in (5 m)
  • Empty weight: 30,328 lb (13,757 kg)
  • Gross weight: 41,500 lb (18,824 kg)
  • Max takeoff weight: 61,795 lb (28,030 kg)
  • Powerplant: 2 × General Electric J79-GE-17A after-burning turbojet engines, 11,905 lbf (52.96 kN) thrust each dry, 17,845 lbf (79.38 kN

Performance

  • Maximum speed: 1,280 kn (1,470 mph, 2,370 km/h) at 40,000 ft 
  • Maximum speed: Mach 2.23
  • Cruise speed: 510 kn (580 mph, 940 km/h)
  • Combat range: 370 nmi (420 mi, 680 km)
  • Ferry range: 1,457 nmi (1,677 mi, 2,699 km)
  • Service ceiling: 60,000 ft (18,000 m)
  • Thrust/weight: 0.86 at loaded weight, 0.58 at MTOW
  • Takeoff roll: 4,490 ft (1,370 m) at 53,814 lb (24,410 kg)
  • Landing roll: 3,680 ft (1,120 m) at 36,831 lb (16,706 kg)
  • Armament

    E-model has a 20 mm (0.787 in) M61A1 Vulcan cannon mounted internally under the nose, 640 roundsUp to 18,650 lb (8,480 kg) of weapons on nine external hardpoints, including general-purpose bombs, cluster bombs, TV- and laser-guided bombs, rocket pods, air-to-ground missiles, anti-ship missiles, gun pods, and nuclear weapons. Reconnaissance, targeting, electronic countermeasures and baggage pods, and external fuel tanks may also be carried.4× AIM-9 Sidewinders on wing pylons, Israeli F-4 Kurnass 2000 carried Python-3, Japanese F-4EJ Kai carry AAM-3AIM-7 Sparrow in fuselage recesses.

Aircrafttoaal encyclopedia

"Speed is life" was F-4 pilots' slogan. The Phantom's greatest advantage in air combat was acceleration and thrust, which permitted a skilled pilot to engage and disengage from the fight at will. MiGs usually could outturn the F-4 because of the high drag on its airframe; as a massive fighter aircraft designed to fire radar-guided missiles from beyond visual range, the F-4 lacked the agility of its Soviet opponents and was subject to adverse yaw during hard maneuvering.