The McDonnell Douglas F-4 Phantom II[N 1] is a tandem, two-seat, twin-engine, all-weather, long-range supersonic jet interceptor fighter/fighter-bomber originally developed for the United States Navy by McDonnell Aircraft.[1] 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 respective air wings.[2]
The Phantom is a large fighter with a top speed of over Mach 2.2. It can carry over 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 a M61 Vulcan rotary cannon. Beginning in 1959 it set 15 world records for in-flight performance,[3] including an absolute speed record, and an absolute altitude record.[4]
During the Vietnam War the F-4 was used extensively; it served as the principal air superiority fighter for both the Navy and Air Force, and became important in the ground-attack and reconnaissance roles late in the war. The Phantom has the distinction of being the last U.S. fighter flown to attain ace status in the 20th century. During the Vietnam War the USAF had one pilot and two weapon systems officers (WSOs),[5] and the US Navy one pilot and one radar intercept officer (RIO), achieve five aerial kills against other enemy fighter aircraft and become aces in air-to-air combat.[6] 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 and F/A-18 Hornet in the U.S. Navy; and the F/A-18 in the 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 Gulf War, finally leaving service in 1996.[7][8] It was also the only aircraft used by both U.S. flight demonstration teams: the USAF Thunderbirds (F-4E) and the US Navy Blue Angels (F-4J).[2][9][10] 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 in the Iran–Iraq War. Phantoms remain in front line service with seven countries, and in use as an unmanned target in the U.S. Air Force.[11] Phantom production ran from 1958 to 1981, with a total of 5,195 built, making it the most numerous American supersonic military aircraft.[2][12]
Origins
In 1952, McDonnell's Chief of Aerodynamics, Dave Lewis, was appointed by CEO Jim McDonnell to be the company's Preliminary Design Manager.[13] With no new aircraft competitions on the horizon, internal studies concluded the Navy had the greatest need for a new and different aircraft type: an attack fighter.[14]In 1953, McDonnell Aircraft began work on revising its F3H Demon naval fighter, seeking expanded capabilities and better performance. The company developed several projects including a variant powered by a Wright J67 engine,[15] and variants powered by two Wright J65 engines, or two General Electric J79 engines.[16] The J79-powered version promised a top speed of Mach 1.97. On 19 September 1953, McDonnell approached the United States Navy with a proposal for the "Super Demon". Uniquely, the aircraft was to be modular—it could be fitted with one- or two-seat noses for different missions, with different nose cones to accommodate radar, photo cameras, four 20 mm (.79 in) cannon, or 56 FFAR unguided rockets in addition to the nine hardpoints under the wings and the fuselage. The Navy was sufficiently interested to order a full-scale mock-up of the F3H-G/H, but felt that the upcoming Grumman XF9F-9 and Vought XF8U-1 already satisfied the need for a supersonic fighter.[17]
The McDonnell design was therefore reworked into an all-weather fighter-bomber with 11 external hardpoints for weapons and on 18 October 1954, the company received a letter of intent for two YAH-1 prototypes. On 26 May 1955, four Navy officers arrived at the McDonnell offices and, within an hour, presented the company with an entirely new set of requirements. Because the Navy already had the Douglas A-4 Skyhawk for ground attack and F-8 Crusader for dogfighting, the project now had to fulfill the need for an all-weather fleet defense interceptor. A second crewman was added to operate the powerful radar.[1
World records
To show off their new fighter, the Navy led a series of record-breaking flights early in Phantom development:[2] All in all, the Phantom set 16 world records. With the exception of Skyburner, all records were achieved in unmodified production aircraft. Five of the speed records remained unbeaten until the F-15 Eagle appeared in 1975.[3]- Operation Top Flight: On 6 December 1959, the second XF4H-1 performed a zoom climb to a world record 98,557 ft (30,040 m).[4] The previous record of 94,658 ft (28,852 m) was set by a Soviet Sukhoi T-43-1 prototype. Commander Lawrence E. Flint, Jr., USN accelerated his aircraft to Mach 2.5 at 47,000 ft (14,330 m) and climbed to 90,000 ft (27,430 m) at a 45° angle. He then shut down the engines and glided to the peak altitude. As the aircraft fell through 70,000 ft (21,300 m), Flint restarted the engines and resumed normal flight.[26]
- On 5 September 1960, an F4H-1 averaged 1,216.78 mph (1,958.16 km/h) over a 500 km (311 mi) closed-circuit course.[4]
- On 25 September 1960, an F4H-1 averaged 1,390.21 mph (2,237.26 km/h) over a 100 km (62.1 mi) closed-circuit course.[4]
- Operation LANA: To celebrate the 50th anniversary of Naval aviation (L is the Roman numeral for 50 and ANA stood for Anniversary of Naval Aviation) on 24 May 1961, Phantoms flew across the continental United States in under three hours and included several tanker refuelings. The fastest of the aircraft averaged 869.74 mph (1,400.28 km/h) and completed the trip in 2 hours 47 minutes, earning the pilot (and future NASA Astronaut), Lieutenant Richard Gordon, USN and RIO, Lieutenant Bobbie Young, USN, the 1961 Bendix trophy.[4][27][28][29]
- Operation Sageburner: On 28 August 1961, a Phantom averaged 902.769 mph (1,452.826 km/h) over a 3 mi (4.82 km) course flying below 125 feet (38.1 m) at all times.[4] Commander J.L. Felsman, USN was killed during the first attempt at this record on 18 May 1961 when his aircraft disintegrated in the air after pitch damper failure.[30]
- Operation Skyburner: On 22 December 1961, a modified Phantom with water injection set an absolute world record speed of 1,606.342 mph (2,585.086 km/h).[4]
- On 5 December 1961, another Phantom set a sustained altitude record of 66,443.8 feet (20,252 m).[4]
- Operation High Jump: A series of time-to-altitude records was set in early 1962: 34.523 seconds to 3,000 meters (9,840 ft), 48.787 seconds to 6,000 meters (19,700 ft), 61.629 seconds to 9,000 meters (29,500 ft), 77.156 seconds to 12,000 meters (39,400 ft), 114.548 seconds to 15,000 meters (49,200 ft), 178.5 seconds to 20,000 meters (65,600 ft), 230.44 seconds to 25,000 metres (82,000 ft), and 371.43 seconds to 30,000 metres (98,400 ft).[3
Variants
- F-4A, B, J, N and S
- Variants for the U.S. Navy and the U.S. Marines. F-4B was upgraded to F-4N, and F-4J was upgraded to F-4S.
- F-110 Spectre, F-4C, D and E
- Variants for the U.S. Air Force. F-4E introduced an internal M61 Vulcan cannon. The F-4D and E were the most numerously built, widely exported, and also extensively used under the Semi Automatic Ground Environment (SAGE) U.S. air defense system.
- F-4G Wild Weasel V
- A dedicated SEAD variant with updated radar and avionics, converted from F-4E. The designation F-4G was applied earlier to an entirely different Navy Phantom.
- F-4K and M
- Variants for the British military re-engined with Rolls-Royce Spey turbofans.
- F-4EJ
- Simplified F-4E exported to and license-built in Japan.
- F-4F
- Simplified F-4E exported to Germany.
- QF-4B, E, G, N and S
- Retired aircraft converted into remote-controlled target drones used for weapons and defensive systems research.
- RF-4B, C, and E
- Tactical reconnaissance variants
- General characteristics
- Crew: 2
- Length: 63 ft 0 in (19.2 m)
- Wingspan: 38 ft 4.5 in (11.7 m)
- Height: 16 ft 6 in (5.0 m)
- Wing area: 530.0 ft² (49.2 m²)
- Airfoil: NACA 0006.4–64 root, NACA 0003-64 tip
- Empty weight: 30,328 lb (13,757 kg)
- Loaded weight: 41,500 lb (18,825 kg)
- Max. takeoff weight: 61,795 lb (28,030 kg)
- Powerplant: 2 × General Electric J79-GE-17A axial compressor turbojets, 11,905 lbf dry thrust (52.9 kN), 17,845 lbf in afterburner (79.4 kN) each
- Zero-lift drag coefficient: 0.0224
- Drag area: 11.87 ft² (1.10 m²)
- Aspect ratio: 2.77
- Fuel capacity: 1,994 U.S. gal (7,549 L) internal, 3,335 U.S. gal (12,627 L) with three external tanks (370 U.S. gal (1,420 L) tanks on the outer wing hardpoints and either a 600 or 610 U.S. gal (2,310 or 2,345 L) tank for the centerline station).
- Maximum landing weight: 36,831 lb (16,706 kg)
- Maximum speed: Mach 2.23 (1,472 mph, 2,370 km/h) at 40,000 ft (12,190 m)
- Cruise speed: 506 kn (585 mph, 940 km/h)
- Combat radius: 367 nmi (422 mi, 680 km)
- Ferry range: 1,403 nmi (1,615 mi, 2,600 km) with 3 external fuel tanks
- Service ceiling: 60,000 ft (18,300 m)
- Rate of climb: 41,300 ft/min (210 m/s)
- Wing loading: 78 lb/ft² (383 kg/m²)
- lift-to-drag: 8.58
- 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)
- Up 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 (UK Phantoms 6 × Matra rocket pods with 18 × SNEB 68 mm rockets each), air-to-ground missiles, anti-runway weapons, anti-ship missiles, targeting pods, reconnaissance pods, and nuclear weapons. Baggage pods and external fuel tanks may also be carried.
- 4× AIM-7 Sparrow in fuselage recesses plus 4 × AIM-9 Sidewinders on wing pylons; upgraded Hellenic F-4E and German F-4F ICE carry AIM-120 AMRAAM, Japanese F-4EJ Kai carry AAM-3, Hellenic F-4E will carry IRIS-T in future. Iranian F-4s could potentially carry Russian and Chinese missiles. UK Phantoms carried Skyflash missiles[125]
- 1× 20 mm (0.787 in) M61 Vulcan 6-barrel gatling cannon, 640 rounds
- 4× AIM-9 Sidewinder, Python-3 (F-4 Kurnass 2000), IRIS-T (F-4E AUP Hellenic Air Force)
- 4× AIM-7 Sparrow, AAM-3(F-4EJ Kai)
- 4× AIM-120 AMRAAM for F-4F ICE, F-4E AUP (Hellenic Air Force)
- 6× AGM-65 Maverick
- 4× AGM-62 Walleye
- 4× AGM-45 Shrike, AGM-88 HARM, AGM-78 Standard ARM
- 4× GBU-15
- 18× Mk.82, GBU-12
- 5× Mk.84, GBU-10, GBU-14
- 18× CBU-87, CBU-89, CBU-58
- Nuclear weapons, including the B28EX, B61, B43 and B57
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