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

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. Proving highly adaptable, it first entered service with the Navy in 1961 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.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.

Manufacturer: McDonnell Aircraft Corporation, McDonnell Douglas
First flight: 27 May 1958
Introduction: 1961
Retired: 1994 (United Kingdom), 1996 (U.S. combat use), 2013 (Germany), 2021 (Japan)
Status: In limited service
Primary users: United States Air Force, United States Navy, United States Marine Corps, Iranian Air Force
Produced: 1958–1981
Number built: 5,195

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)
Wing area: 530 sq ft (49.2 m2)
Aspect ratio: 2.77
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)
Maximum landing weight: 36,831 lb (16,706 kg)
Fuel capacity: 1,994 US gal (1,660 imp gal; 7,550 l) internal, 3,335 US gal (2,777 imp gal; 12,620 l) with 2x 370 US gal (310 imp gal; 1,400 l) external tanks on the outer wing hardpoints and either a 600 or 610 US gal (500 or 510 imp gal; 2,300 or 2,300 l) tank for the center-line station.
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) with afterburner

Performance

Maximum speed: 1,280 kn (1,470 mph, 2,370 km/h) at 40,000 ft (12,000 m)
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)
Rate of climb: 41,300 ft/min (210 m/s)
Lift-to-drag: 8.58
Wing loading: 78 lb/sq ft (380 kg/m2)
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)

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