F-4 Phantom II
| F-4 Phantom II | ||
|---|---|---|
 USAF F-4 Phantom II | ||
| Description | ||
| Role | All-weather fighter-bomber | |
| Crew | Two | |
| Dimensions | ||
| Length | 62 ft 11 in | 19.1 m |
| Wingspan | 38 ft 11 in | 11.8 m |
| Height | 16 ft 5 in | 5 m |
| Wing area | 530 ft² | 49.2 mÃÂò |
| Weights | ||
| Empty | 28,496 lb | 12,926 kg |
| Gross | 51,441 lb | 23,333 kg |
| Maximum take-off | 58,000 lb | 26,308 kg |
| Powerplant | ||
| Engines | Two General Electric J79 turbojet engines | |
| Thrust | 17,900 lb | 80 kN |
| Performance | ||
| Maximum speed | 1,433 mph at 48,000 ft | 2,306 km/h at 14,5000 m |
| Combat range | 538 miles | 865 km |
| Ferry range | 1,926 miles | 3,100 km |
| Service ceiling | 60,000 ft | 18,000 m |
| Rate of climb | 40,550 ft/min | 12,360 m/min |
| Armament | ||
| Guns | GAU-4 20 mm Vulcan, six barreled gattling gun (6,000 rounds/min). | |
| Bombs | four pylon bomb racks (12,500 lb/5,670 kg) 15 CBU-52, 15 CBU-58, 15 CBR-71, 15 CBU-87, 15 CBU-89, 12 MK-20, 6 BL-755 | |
The F-4 Phantom II is a two-place (tandem), supersonic, long-range, all-weather fighter-bomber built by McDonnell Douglas Corporation. It was operated by the US Navy, the USMC and later the USAF, from 1961 until 1995. It is still in service with other nations.
Its primary mission capabilities are: long range, high-altitude intercepts utilizing air-to-air missiles as primary armament; a 20mm M61 Vulcan cannon as secondary armament; long-range attack missions utilizing conventional or nuclear weapons as a primary armament; and close air support missions utilizing a choice of bombs, rockets and missiles as primary armament. It was one of the few aircraft types that have served in the US Navy, USMC and USAF. It was one of the longest serving military aircraft post-war.
First flown in May 1958, the Phantom II originally was developed for U.S. Navy fleet defense and entered service in 1961. The USAF evaluated it (as the F-110A Spectre) for close air support, interdiction, and counter-air operations and, in 1962, approved a USAF version. The USAF's Phantom II, designated F-4C, made its first flight on May 27, 1963. Production deliveries began in November 1963.
In its air-to-ground role the F-4 can carry twice the normal bomb load of a WW II B-17 Flying Fortress. USAF F-4s also flew reconnaissance and "Wild Weasel" air-defence suppression missions. Phantom II production ended in 1979 after over 5,000 had been built--more than 2,800 for the USAF, about 1,200 for the Navy and Marine Corps, and the rest for friendly foreign nations.
In 1965 the first USAF Phantom IIs were sent to Vietnam. Early versions (F-4A to F-4D) lacked any gun armament. Coupled with the unreliability of the air-to-air missiles AIM-7 Sparrow AIM-9 Sidewinder at the time, this major drawback resulted in the aircraft loss after they ran out of missiles. During the course of the Vietnam War, its contemporaries, the MiG-19 and MiG-21, inflicted heavy losses on the F-4s when the American aircrafts were ambushed after returning from bombing assignments. This prompted the USAF to introduce the F-4E variant, which added a M61 Vulcan cannon in the nose of the aircraft, below the radome.
This later version was the mainstay of the USAF Phantom II forces and served with the air forces of many countries including Australia, Greece, Israel, Iran, Japan, Spain, South Korea, Turkey and West Germany. F-4E did not serve in USN or USMC, but an improved variant of F-4B, the F-4J replaced earlier Phantom II variants in these services. F-4J lacked gun armament either.
The German Version (F-4F) will be used until the Eurofighter_Typhoon is produced in sufficient mumbers. The newer AN/APG-65 radar (same as in the F/A-18) was installed in order to use AIM-120 AMRAAM air-to-air missiles.
The United Kingdom bought the aircraft for use with the Royal Air Force and Fleet Air Arm; British versions were fitted with the larger but more powerful Rolls-Royce Spey engine and were designated F-4K. Fleet Air Arm Phantoms were fitted with a telescoping front undercarriage leg allowing the nose to be raised up high, the increased angle of attack being necessary for catapult launches from the small British carriers.
The last of the F-4s were retired from duty with the US military in 1995; however the aircraft still sees use in a training role, as a drone, and in service to other nations. The UK retired its last Phantoms in 1993.
See also the FH-1 Phantom.
General Characteristics:
Variants
Units Using the F-4
United States Navy
United States Marine Corps
United States Air Force
Royal Air Force
Fleet Air Arm
Royal Australian Air Force
Luftwaffe
Israeli Air Force
Egyptian Air Force
Greek Air Force
Iranian Air Force
| Related content | |
|---|---|
| Similar Aircraft | |
| Designation Series (USN Pre-1962) | FH - F2H - F3H - F4H |
| Designation Series (USAF Pre-1962) | F-106 - YF-107 - XF-108 - F-110 - F-111 - F-117 |
| Designation Series (Post-1962) | F-1 - F-2 - F-3 - F-4 - F-5 - F-6 - F-7 |
| Related Lists | List of military aircraft of the United States - List of fighter aircraft |
| List of Aircraft - Aircraft Manufacturers - Aircraft Engines - Aircraft Engine Manufacturers |
| Airlines - Air Forces - Aircraft Weapons - Missiles - Years in Aviation |