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McDonnell Douglas F-4 Phantom II
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The McDonnell Douglas F-4 Phantom II[N 1] is an American tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber that was developed by McDonnell Aircraft for the United States Navy.[4] It entered service with the Navy in 1961,[5] then was adopted by the United States Marine Corps, and the United States Air Force, and within a few years became a major part of their air arms.[6] A total of 5,195 Phantoms were built from 1958 to 1981, making it the most-produced American supersonic military aircraft in history and a signature combat aircraft of the Cold War.[6][7]
Key Information
The Phantom is a large fighter with a top speed of over Mach 2.2. It can carry more than 18,000 pounds (8,400 kg) of weapons on nine external hardpoints, including air-to-air missiles, air-to-ground missiles, and various bombs.[8] Like other interceptors of its time, the F-4 was initially designed without an internal cannon, but some later models incorporated an internal M61 Vulcan rotary cannon. Beginning in 1959, it set 15 world records for in-flight performance,[9] including an absolute speed record and an absolute altitude record.[10]
The F-4 was used extensively during the Vietnam War, first as the principal air superiority fighter for the U.S. Air Force, Navy, and Marine Corps, and later as a ground-attack and aerial reconnaissance aircraft. During the Vietnam War, all five American servicemen who became aces – one U.S. Air Force pilot and two weapon systems officers (WSOs),[11] one U.S. Navy pilot and one radar intercept officer (RIO) – did so in F-4s.[12] The Phantom remained a major part of U.S. military air power into the 1980s, when it was gradually replaced by more modern aircraft such as the F-15 Eagle and F-16 Fighting Falcon in the U.S. Air Force, the F-14 Tomcat in the U.S. Navy, and the F/A-18 Hornet in the U.S. Navy and U.S. Marine Corps.
The Phantom was used for reconnaissance and Wild Weasel (Suppression of Enemy Air Defenses) missions in the 1991 Gulf War, and finally left combat service in 1996.[13][14] It was 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).[6][15][16] 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. The F-4 remains in active service with the Hellenic Air Force[17] and the Turkish Air Force. Turkey's most recently upgraded F-4E Terminator variant is to remain in service until at least 2030.[18]
Development
[edit]Origins
[edit]In 1952, McDonnell's Chief of Aerodynamics, Dave Lewis, was appointed by CEO Jim McDonnell to be the company's preliminary design manager.[19] 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.[20]

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,[21] and variants powered by two Wright J65 engines, or two General Electric J79 engines.[22] 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, as 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.[23]
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. Then 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;[4] designers believed that air combat in the next war would overload solo pilots with information.[24]
XF4H-1 prototype
[edit]
The XF4H-1 was designed to carry four semi-recessed AAM-N-6 Sparrow III radar-guided missiles, and to be powered by two J79-GE-8 engines. As in the McDonnell F-101 Voodoo, the engines sat low in the fuselage to maximize internal fuel capacity and ingested air through fixed geometry intakes. The thin-section wing had a leading edge sweep of 45° and was equipped with blown flaps for better low-speed handling.[25]
Wind tunnel testing had revealed lateral instability, requiring the addition of 5° dihedral to the wings.[26] To avoid redesigning the titanium central section of the aircraft, McDonnell engineers angled up only the outer portions of the wings by 12°, which averaged to the required 5° over the entire wingspan. The wings also received the distinctive "dogtooth" for improved control at high angles of attack. The all-moving tailplane was given 23° of anhedral to improve control at high angles of attack, while still keeping the tailplane clear of the engine exhaust.[25] In addition, air intakes were equipped with one fixed ramp and one variable geometry ramp with angle scheduled to give maximum pressure recovery between Mach 1.4 and Mach 2.2. Airflow matching between the inlet and engine was achieved by bypassing the engine as secondary air into the exhaust nozzle. All-weather intercept capability was achieved with the AN/APQ-50 radar. To meet requirements for carrier operations, the landing gear was designed to withstand landings with a maximum sink rate of 23 ft/s (7 m/s), while the nose strut could extend by 20 in (51 cm) to increase angle of attack on the catapult portion of a takeoff.[26]

On 25 July 1955, the Navy ordered two XF4H-1 test aircraft and five YF4H-1 pre-production examples. The Phantom made its maiden flight on 27 May 1958 with Robert C. Little at the controls. A hydraulic problem precluded the retraction of the landing gear, but subsequent flights went more smoothly. Early testing resulted in redesign of the air intakes, including the distinctive addition of 12,500 holes to "bleed off" the slow-moving boundary layer air from the surface of each intake ramp. Series production aircraft also featured splitter plates to divert the boundary layer away from the engine intakes. The aircraft was soon in competition with the XF8U-3 Crusader III. Due to cockpit workload, the Navy wanted a two-seat aircraft and on 17 December 1958 the F4H was declared the winner. Delays with the J79-GE-8 engines meant that the first production aircraft were fitted with J79-GE-2 and −2A engines, each having 16,100 lbf (71.8 kN) of afterburning thrust. In 1959, the Phantom began carrier suitability trials with the first complete launch-recovery cycle performed on 15 February 1960 from Independence.[26]
There were proposals to name the F4H "Satan" and "Mithras".[26] In the end, the aircraft was given the less controversial name "Phantom II", the first "Phantom" being another McDonnell jet fighter, the FH-1 Phantom. The Phantom II was briefly given the designation F-110A and named "Spectre" by the USAF[27] and the Tri-Service aircraft designation system, F-4, was adopted in September 1962.
Production
[edit]
Early in production, the radar was upgraded to the Westinghouse AN/APQ-72, an AN/APQ-50 with a larger radar antenna, necessitating the bulbous nose, and the canopy was reworked to improve visibility and make the rear cockpit less claustrophobic.[28] During its career the Phantom underwent many changes in the form of numerous variants developed.
The USN operated the F4H-1 (re-designated F-4A in 1962) with J79-GE-2 and -2A engines of 16,100 lbf (71.62 kN) thrust and later builds receiving -8 engines. A total of 45 F-4As were built; none saw combat, and most ended up as test or training aircraft.[29] The USN and USMC received the first definitive Phantom, the F-4B which was equipped with the Westinghouse APQ-72 radar (pulse only), a Texas Instruments AN/AAA-4 Infrared search and track pod under the nose, an AN/AJB-3 bombing system and powered by J79-GE-8,-8A and -8B engines of 10,900 lbf (48.5 kN) dry and 16,950 lbf (75.4 kN) afterburner (reheat) with the first flight on 25 March 1961. 649 F-4Bs were built with deliveries beginning in 1961 and VF-121 Pacemakers receiving the first examples at NAS Miramar.[29]
The USAF received Phantoms as the result of Defense Secretary Robert McNamara's push to create a unified fighter for all branches of the US military. After an F-4B won the "Operation Highspeed" fly-off against the Convair F-106 Delta Dart, the USAF borrowed two Naval F-4Bs, temporarily designating them F-110A in January 1962, and developed requirements for their own version. Unlike the US Navy's focus on air-to-air interception in the Fleet Air Defense (FAD) mission, the USAF emphasized both an air-to-air and an air-to-ground fighter-bomber role. With McNamara's unification of designations on 18 September 1962, the Phantom became the F-4 with the naval version designated F-4B and USAF F-4C. The first Air Force Phantom flew on 27 May 1963, exceeding Mach 2 on its maiden flight.[30]
The F-4J improved both air-to-air and ground-attack capability; deliveries begun in 1966 and ended in 1972 with 522 built.[31] It was equipped with J79-GE-10 engines with 17,844 lbf (79.374 kN) thrust, the Westinghouse AN/AWG-10 Fire Control System (making the F-4J the first fighter in the world with operational look-down/shoot-down capability),[32] a new integrated missile control system and the AN/AJB-7 bombing system for expanded ground attack capability.[33]
The F-4N (updated F-4Bs) with smokeless engines and F-4J aerodynamic improvements started in 1972 under a U.S. Navy-initiated refurbishment program called "Project Bee Line"[34] with 228 converted by 1978. The F-4S model resulted from the refurbishment of 265 F-4Js with J79-GE-17 smokeless engines of 17,900 lbf (79.379 kN), AWG-10B radar with digitized circuitry for improved performance and reliability, Honeywell AN/AVG-8 Visual Target Acquisition Set or VTAS (world's first operational Helmet Sighting System), classified avionics improvements, airframe reinforcement and leading edge slats for enhanced maneuvering.[35] The USMC also operated the RF-4B with reconnaissance cameras with 46 built;[36] the RF-4B flew alone and unarmed, with a requirement to fly straight and level at 5,000 feet while taking photographs. They relied on the shortcomings of the anti-aircraft defenses to survive as they were unable to make evasive maneuvers.[24]
Phantom II production ended in the United States in 1979 after 5,195 had been built (5,057 by McDonnell Douglas and 138 in Japan by Mitsubishi). Of these, 2,874 went to the USAF, 1,264 to the Navy and Marine Corps, and the rest to foreign customers.[6] The last U.S.-built F-4 went to South Korea, while the last F-4 built was an F-4EJ built by Mitsubishi Heavy Industries in Japan and delivered on 20 May 1981.[37] As of 2008, 631 Phantoms were in service worldwide,[38] while the Phantoms were in use as a target drone (specifically QF-4Cs) operated by the U.S. military until 21 December 2016, when the Air Force officially ended use of the type.[39]
World records
[edit]
To show off their new fighter, the Navy led a series of record-breaking flights early in Phantom development:[6] All in all, the Phantom set 16 world records. Five of the speed records remained unbeaten until the F-15 Eagle appeared in 1975.[9]
- 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).[10][40] Commander Lawrence E. Flint Jr., USN accelerated his aircraft to Mach 2.5 (2,660 km/h; 1,650 mph) 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.[41]
- 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.[10]
- On 25 September 1960, an F4H-1F averaged 1,390.24 mph (2,237.37 km/h) over a 100 km (62.1 mi) closed-circuit course.[10] FAIRecord File Number 8898.
- 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[42] Richard Gordon, USN and RIO, Lieutenant Bobbie Young, USN, the 1961 Bendix trophy.[10][43][44][45]
- Operation Sageburner: On 28 August 1961, a F4H-1F Phantom II averaged 1,452.777 kilometers per hour (902.714 miles per hour) over a 3 mi (4.82 km) course flying below 125 feet (38.1 m) at all times.[10] 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.[46]
- Operation Skyburner: On 22 November 1961, a modified Phantom with water injection, piloted by Lt. Col. Robert B. Robinson, set an absolute world record average speed over a 20-mile (32.2 km) long 2-way straight course of 1,606.342 mph (2,585.086 km/h).[10][47][48][49]
- On 5 December 1961, another Phantom set a sustained altitude record of 66,443.8 feet (20,252 m).[10]
- Project High Jump: A series of time-to-altitude records was set in early 1962: 34.523 seconds to 3,000 m (9,840 ft), 48.787 seconds to 6,000 m (19,700 ft), 61.629 seconds to 9,000 m (29,500 ft), 77.156 seconds to 12,000 m (39,400 ft), 114.548 seconds to 15,000 m (49,200 ft), 178.5 s to 20,000 m (65,600 ft), 230.44 s to 25,000 m (82,000 ft), and 371.43 s to 30,000 m (98,400 ft).[50] All High Jump records were set by F4H-1 production number 108 (Bureau Number 148423).[51][52][53][54] Two of the records were set by future distinguished NASA astronaut LCdr John Young.[55][56]
Design
[edit]Overview
[edit]The F-4 Phantom is a tandem-seat fighter-bomber designed as a carrier-based interceptor to fill the U.S. Navy's fleet defense fighter role. Innovations in the F-4 included use of pulse-doppler radar (only on late variants such as the F-4F) and extensive use of titanium in its airframe.[57]
Despite imposing dimensions and a maximum takeoff weight of over 60,000 lb (27,000 kg),[58] the F-4 has a top speed of Mach 2.23 and an initial climb rate of over 41,000 ft/min (210 m/s).[59] The F-4's nine external hardpoints have a capability of up to 18,650 pounds (8,480 kg) of weapons, including air-to-air and air-to-surface missiles, and unguided, guided, and thermonuclear weapons.[60] Like other interceptors of its day, the F-4 was designed without an internal cannon.[61]
The baseline performance of a Mach 2-class fighter with long range and a bomber-sized payload would be the template for the next generation of large and light/middle-weight fighters optimized for daylight air combat.[62]
Flight characteristics
[edit]"Speed is life" was F-4 pilots' slogan, as the Phantom's greatest advantage in air combat was acceleration[24] 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 the Phantom's airframe;[63] 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. Although the F-4 was subject to irrecoverable spins during aileron rolls, pilots reported the aircraft to be very responsive and easy to fly on the edge of its performance envelope. In 1972, the F-4E model was upgraded with leading edge slats on the wing, greatly improving high angle of attack maneuverability at the expense of top speed.[64]
The J79 had a reduced time lag between the pilot advancing the throttle, from idle to maximum thrust, and the engine producing maximum thrust compared to earlier engines. While landing on USS Midway (CV-41) John Chesire's tailhook missed the arresting gear as he (mistakenly) reduced thrust to idle. He then slammed the throttle to full afterburner, the engine's response time being enough to return to full thrust quickly, and he was able get the Phantom airborne again successfully (bolter).[24] The J79 produced noticeable amounts of black smoke (at mid-throttle/cruise settings), a severe disadvantage in that it made it easier for the enemy to spot the aircraft.[65] Two decades after the aircraft entered service[24] this was solved on the F-4S, which was fitted with the −10A engine variant with a smokeless combustor.[66]
The lack of an internal gun "was the biggest mistake on the F-4", Chesire said; "Bullets are cheap and tend to go where you aim them. I needed a gun, and I really wished I had one." Marine Corps General John R. Dailey recalled that "everyone in RF-4s wished they had a gun on the aircraft."[24] For a brief period, doctrine held that turning combat would be impossible at supersonic speeds and little effort was made to teach pilots air combat maneuvering. In reality, engagements quickly became subsonic, as pilots would slow down in an effort to get behind their adversaries. Furthermore, the relatively new heat-seeking and radar-guided missiles at the time were frequently reported as unreliable and pilots had to fire multiple missiles just to hit one enemy fighter. To compound the problem, rules of engagement in Vietnam precluded long-range missile attacks in most instances, as visual identification was normally required. Many pilots found themselves on the tail of an enemy aircraft, but too close to fire short-range Falcons or Sidewinders. Although by 1965 USAF F-4Cs began carrying SUU-16 external gunpods containing a 20 mm (.79 in) M61A1 Vulcan Gatling cannon, USAF cockpits were not equipped with lead-computing gunsights until the introduction of the SUU-23, virtually assuring a miss in a maneuvering fight. Some Marine Corps aircraft carried two pods for strafing. In addition to the loss of performance due to drag, combat showed the externally mounted cannon to be inaccurate unless frequently boresighted, yet far more cost-effective than missiles. The lack of a cannon was finally addressed by adding an internally mounted 20 mm (.79 in) M61A1 Vulcan on the F-4E.[64]
Costs
[edit]| F-4C | RF-4C | F-4D | F-4E | |
|---|---|---|---|---|
| Unit R&D cost | – | 61,200 (1965) by 1973 610,643 (current) by 1973 |
– | 22,700 (1965) by 1973 226,497 (current) by 1973 |
| Airframe | 1,388,725 (1965) 13,856,455 (current) |
1,679,000 (1965) 16,752,768 (current) |
1,018,682 (1965) 10,164,230 (current) |
1,662,000 (1965) 16,583,145 (current) |
| Engines | 317,647 (1965) 3,169,426 (current) |
276,000 (1965) 2,753,880 (current) |
260,563 (1965) 2,599,852 (current) |
393,000 (1965) 3,921,285 (current) |
| Electronics | 52,287 (1965) 521,711 (current) |
293,000 (1965) 2,923,503 (current) |
262,101 (1965) 2,615,198 (current) |
299,000 (1965) 2,983,370 (current) |
| Armament | 139,706 (1965) 1,393,962 (current) |
73,000 (1965) 728,381 (current) |
133,430 (1965) 1,331,341 (current) |
111,000 (1965) 1,107,539 (current) |
| Ordnance | – | – | 6,817 (1965) 68,019 (current) |
8,000 (1965) 79,823 (current) |
| Flyaway cost | 1.9 million (1965) 19 million (current) |
2.3 million (1965) 22.9 million (current) |
1.7 million (1965) 17 million (current) |
2.4 million (1965) 23.9 million (current) |
| Modification costs | 116,289 (1965) by 1973 1,160,311 (current) by 1973 |
55,217 (1965) by 1973 550,946 (2008) by 1973 |
233,458 (1965) by 1973 2,329,403 (current) by 1973 |
7,995 (1965) by 1973 79,773 (current) by 1973 |
| Cost per flying hour | 924 (1965) 9,220 (2008) |
867 (1965) 8,651 (current) |
896 (1965) 8,940 (current) |
867 (1965) 8,651 (current) |
| Maintenance cost per flying hour | 545 (1965) 5,438 (current) | |||
Note: Original amounts were in 1965 U.S. dollars.[67] The figures in these tables have been adjusted for inflation to the current year.
Operational history
[edit]United States Navy
[edit]
On 30 December 1960, VF-121 Pacemakers at NAS Miramar became the first Phantom operator with its F4H-1Fs (F-4As). The VF-74 Be-devilers at NAS Oceana became the first deployable Phantom squadron when it received its F4H-1s (F-4Bs) on 8 July 1961.[68] The squadron completed carrier qualifications in October 1961 and Phantom's first full carrier deployment between August 1962 and March 1963 aboard Forrestal.[69] The second deployable U.S. Atlantic Fleet squadron to receive F-4Bs was the VF-102 Diamondbacks, who promptly took their new aircraft on the shakedown cruise of Enterprise.[70] The first deployable U.S. Pacific Fleet squadron to receive the F-4B was the VF-114 Aardvarks, which participated in the September 1962 cruise aboard USS Kitty Hawk.[68]
By the time of the Tonkin Gulf incident, 13 of 31 deployable navy squadrons were armed with the type. F-4Bs from Constellation made the first Phantom combat sortie of the Vietnam War on 5 August 1964, flying bomber escort in Operation Pierce Arrow.[71] Navy fighter pilots were unused to flying with a non-pilot RIO, but learned from air combat in Vietnam the benefits of the GiB "guy in back" or "voice in the luggage compartment" helping with the workload.[24] The first Phantom air-to-air victory of the war took place on 9 April 1965 when an F-4B from VF-96 Fighting Falcons piloted by Lieutenant (junior grade) Terence M. Murphy and his RIO, Ensign Ronald Fegan, shot down a Chinese MiG-17. The Phantom was then shot down, probably by an AIM-7 Sparrow from one of its wingmen.[26] There continues to be controversy over whether the Phantom was shot down by MiG guns or, as enemy reports later indicated, an AIM-7 Sparrow III from one of Murphy's and Fegan's wingmen.[72] On 17 June 1965, an F-4B from VF-21 Freelancers piloted by Commander Louis Page and Lieutenant John C. Smith shot down the first North Vietnamese MiG of the war.[73][74]
On 10 May 1972, Lieutenant Randy "Duke" Cunningham and Lieutenant (junior grade) William P. Driscoll flying an F-4J, call sign Showtime 100, shot down three MiG-17s to become the first American flying aces of the war. Their fifth victory was believed at the time to be over a mysterious North Vietnamese ace, Colonel Nguyen Toon, now considered mythical. On the return flight, the Phantom was damaged by an enemy surface-to-air missile. To avoid being captured, Cunningham and Driscoll flew their burning aircraft using only the rudder and afterburner (the damage to the aircraft rendered conventional control nearly impossible), until they could eject over water.[12]

During the war, U.S. Navy F-4 Phantom squadrons participated in 84 combat tours with F-4Bs, F-4Js, and F-4Ns. The Navy claimed 40 air-to-air victories at a cost of 73 Phantoms lost in combat (seven to enemy aircraft, 13 to SAMs and 53 to AAA). An additional 54 Phantoms were lost in mishaps.[75]
In 1984, all Navy F-4Ns were retired from Fleet service in deployable USN squadrons and by 1987 the last F-4Ss were retired from deployable USN squadrons. On 25 March 1986, an F-4S belonging to the VF-151 Vigilantes, became the last active duty U.S. Navy Phantom to launch from an aircraft carrier, in this case, Midway. On 18 October 1986, an F-4S from the VF-202 Superheats, a Naval Reserve fighter squadron, made the last-ever Phantom carrier landing while operating aboard America. In 1987, the last of the Naval Reserve-operated F-4S aircraft were replaced by F-14As. The last Phantoms in service with the Navy were QF-4N and QF-4S target drones operated by the Naval Air Warfare Center at NAS Point Mugu, California.[26] These were subsequently retired in 2004.[76]
United States Marine Corps
[edit]
The Marine Corps received its first F-4Bs in June 1962, with the Black Knights of VMFA-314 at Marine Corps Air Station El Toro, California becoming the first operational squadron. Marine Phantoms of VMFA-323, flying from Puerto Rico, provided air cover during Operation Power Pack for the evacuation of US citizens from the Dominican Republic[77] and assisted the 508th Infantry Regiment in taking and securing a position east of the Duarte bridge. Marine Phantoms from VMFA-531 Grey Ghosts were assigned to Da Nang Air Base on South Vietnam's northeast coast on 10 May 1965 and were initially assigned to provide air defense for the USMC. They soon began close air support missions (CAS) and VMFA-314, VMFA-232 Red Devils, VMFA-323 Death Rattlers and VMFA-542 Tigers soon arrived at the primitive airfield.[78] Marine F-4 pilots claimed three enemy MiGs (two while on exchange duty with the USAF) at the cost of 75 aircraft lost in combat, mostly to ground fire, and four in accidents.[citation needed]
Marine Phantoms from VMFA-323 and VMFA-531 operating from the USS Coral Sea participated in Operation Eagle Claw, the attempted rescue of American hostages from Iran, with orders to shoot down any Iranian aircraft. The Phantoms were painted with an orange stripe enclosed by two black stripes in order to distinguish the American F-4s from the Iranian F-4s.[79][80] The operation was called off in the early stages of execution.
The VMCJ-1 Golden Hawks (later VMAQ-1 and VMAQ-4 which had the old RM tailcode) flew the first photo recon mission with an RF-4B variant on 3 November 1966 from Da Nang and remained there until 1970 with no RF-4B losses and only one aircraft damaged by anti-aircraft artillery (AAA) fire.[81] VMCJ-2 and VMCJ-3 (now VMAQ-3) provided aircraft for VMCJ-1 in Da Nang and VMFP-3 was formed in 1975 at MCAS El Toro, CA consolidating all USMC RF-4Bs in one unit that became known as "The Eyes of the Corps." VMFP-3 disestablished in August 1990 after the Advanced Tactical Airborne Reconnaissance System was introduced for the F/A-18D Hornet.[29]
The F-4 continued to equip fighter-attack squadrons in both active and reserve Marine Corps units throughout the 1960s, 1970s and 1980s and into the early 1990s. In the early 1980s, these squadrons began to transition to the F/A-18 Hornet, starting with the same squadron that introduced the F-4 to the Marine Corps, VMFA-314 at MCAS El Toro, California. On 18 January 1992, the last Marine Corps Phantom, an F-4S in the Marine Corps Reserve, was retired by the Cowboys of VMFA-112 at NAS Dallas, Texas, after which the squadron was re-equipped with F/A-18 Hornets.[82]
United States Air Force
[edit]| Aircraft | Weapons/Tactics | MiG-17 | MiG-19 | MiG-21 | Total |
|---|---|---|---|---|---|
| F-4C | AIM-7 Sparrow | 4 | 0 | 10 | 14 |
| AIM-9 Sidewinder | 12 | 0 | 10 | 22 | |
| 20 mm gunpod | 3 | 0 | 1 | 4 | |
| Maneuvering tactics | 2 | 0 | 0 | 2 | |
| F-4D | AIM-4 Falcon | 4 | 0 | 1 | 5 |
| AIM-7 Sparrow | 4 | 2 | 20 | 26 | |
| AIM-9 Sidewinder | 0 | 2 | 3 | 5 | |
| 20 mm gunpod | 4.5 | 0 | 2 | 6.5 | |
| Maneuvering tactics | 0 | 0 | 2 | 2 | |
| F-4E | AIM-7 Sparrow | 0 | 2 | 8 | 10 |
| AIM-9 Sidewinder | 0 | 0 | 4 | 4 | |
| AIM-9 and 20 mm gunpod | 0 | 0 | 1 | 1 | |
| 20 mm gunpod | 0 | 1 | 4 | 5 | |
| Maneuvering tactics | 0 | 1 | 0 | 1 | |
| Total | 33.5 | 8 | 66 | 107.5 | |
In USAF service, the F-4 was initially designated the F-110A[83] prior to the introduction of the 1962 United States Tri-Service aircraft designation system. The USAF quickly embraced the design and became the largest Phantom user. The first Phantoms that the USAF operated were F-4Bs loaned from the Navy, with 27 jets delivered to the 4453rd Combat Crew Training Wing at MacDill Air Force Base, Florida, in November 1963. The first operational unit was the 12th Tactical Fighter Wing, who received the USAF's first F-4Cs in January 1964, achieving initial operational capability (IOC) in October 1964.[84] The first USAF Phantoms to participate in the Vietnam War were F-4Cs from the 45th Tactical Fighter Squadron, who deployed to Ubon Royal Thai Air Force Base, Thailand, in April 1965.[84][85][86]
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;[24] 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.[87][24]
On 10 July 1965, F-4Cs of the 45th TFS, 15th TFW,[88] scored the USAF's first victories against North Vietnamese MiG-17s using AIM-9 Sidewinder air-to-air missiles.[89] On 26 April 1966, an F-4C from the 480th Tactical Fighter Squadron scored the first aerial victory by a U.S. aircrew over a North Vietnamese MiG-21 "Fishbed".[90] On 24 July 1965, another Phantom from the 45th Tactical Fighter Squadron became the first American aircraft to be downed by an enemy SAM, and on 5 October 1966 an 8th Tactical Fighter Wing F-4C became the first U.S. jet lost to an air-to-air missile, fired by a MiG-21.
On 2 January 1967, F-4Cs of the 8th Tactical Fighter Wing, under the command of Robin Olds, executed Operation Bolo, a response to heavy losses sustained during Operation Rolling Thunder. Olds' and his flight flew out of Ubon in Thailand and simulated an F-105 strike force. In response, the VPAF sent up MiG-21s to shoot down the Phantoms. The ensuing battle resulted in the VPAF losing half of their MiG-21 fleet with no losses from the American side.
Early aircraft suffered from leaks in wing fuel tanks that required re-sealing after each flight and 85 aircraft were found to have cracks in outer wing ribs and stringers.[67] There were also problems with aileron control cylinders, electrical connectors, and engine compartment fires. Reconnaissance RF-4Cs made their debut in Vietnam on 30 October 1965, flying the hazardous post-strike reconnaissance missions. The USAF Thunderbirds used the F-4E from the 1969 season until 1974.[15]

Although the F-4C was essentially identical to the Navy/Marine Corps F-4B in-flight performance and carried the AIM-9 Sidewinder missiles, USAF-tailored F-4Ds initially arrived in June 1967 equipped with AIM-4 Falcons. However, the Falcon, like its predecessors, was designed to shoot down heavy bombers flying straight and level. Its reliability proved no better than others and its complex firing sequence and limited seeker-head cooling time made it virtually useless in combat against agile fighters. The F-4Ds reverted to using Sidewinders under the "Rivet Haste" program in early 1968, and by 1972 the AIM-7E-2 "Dogfight Sparrow" had become the preferred missile for USAF pilots. Like other Vietnam War Phantoms, the F-4Ds were urgently fitted with radar warning receivers to detect the Soviet-built S-75 Dvina SAMs.[91]
From the initial deployment of the F-4C to Southeast Asia, USAF Phantoms performed both air superiority and ground attack roles, supporting not only ground troops in South Vietnam, but also conducting bombing sorties in Laos and North Vietnam. As the F-105 force underwent severe attrition between 1965 and 1968, the bombing role of the F-4 proportionately increased until after November 1970 (when the last F-105D was withdrawn from combat) it became the primary USAF tactical ordnance delivery system. In October 1972 the first squadron of EF-4C Wild Weasel aircraft deployed to Thailand on temporary duty.[92] The "E" prefix was later dropped and the aircraft was simply known as the F-4C Wild Weasel.

Sixteen squadrons of Phantoms were permanently deployed to Indochina between 1965 and 1973, and 17 others deployed on temporary combat assignments.[93] Peak numbers of combat F-4s occurred in 1972, when 353 were based in Thailand.[94] A total of 445 Air Force Phantom fighter-bombers were lost, 370 in combat and 193 of those over North Vietnam (33 to MiGs, 30 to SAMs and 307 to AAA).[94]
The RF-4C was operated by four squadrons,[95] and of the 83 losses, 72 were in combat including 38 over North Vietnam (seven to SAMs and 65 to AAA).[94] By war's end, the U.S. Air Force had lost a total of 528 F-4 and RF-4C Phantoms. When combined with U.S. Navy and Marine Corps losses of 233 Phantoms, 761 F-4/RF-4 Phantoms were lost in the Vietnam War.[96]
On 28 August 1972, Captain Steve Ritchie became the first USAF ace of the war.[11] On 9 September 1972, WSO Capt Charles B. DeBellevue became the highest-scoring American ace of the war with six victories.[11] and WSO Capt Jeffrey Feinstein became the last USAF ace of the war on 13 October 1972.[97] Upon return to the United States, DeBellevue and Feinstein were assigned to undergraduate pilot training (Feinstein was given a vision waiver) and requalified as USAF pilots in the F-4. USAF F-4C/D/E crews claimed 107.5 MiG kills in Southeast Asia (50 by Sparrow, 31 by Sidewinder, five by Falcon, 15.5 by gun, and six by other means).[94]

On 31 January 1972, the 170th Tactical Fighter Squadron, 183d Tactical Fighter Group of the Illinois Air National Guard became the first Air National Guard (ANG) unit to transition to Phantoms from Republic F-84F Thunderstreaks.[98] Phantoms would eventually equip numerous tactical fighter and tactical reconnaissance units in the USAF active, ANG, and Air Force Reserve (AFRES).[99]
On 2 June 1972, a Phantom flying at supersonic speed shot down a MiG-19 over Thud Ridge in Vietnam with its cannon. At a recorded speed of Mach 1.2, Major Phil Handley's shoot down was the first and only recorded gun kill while flying at supersonic speeds.[100][101]
In early December 1989, USAF F-4s, from Clark Air Base, participated in Operation Classic Resolve,[102] President George H.W. Bush's response to the 1989 Philippine coup attempt. The F-4s were ordered to buzz the rebel planes at their base, fire at them if any tried to take off, and shoot them down if they did. The buzzing by the US F-4s soon caused the coup to collapse. On 2 December, President Bush reported that on 1 December, US fighter aircraft from Clark Air Base assisted Philippine President Corazon Aquino's government repel a coup attempt.[103]
On 15 August 1990, 24 F-4G Wild Weasel Vs and six RF-4Cs were deployed to Isa Air Base, Bahrain, for Operation Desert Storm. The F-4G was the only aircraft in the USAF inventory equipped for the Suppression of Enemy Air Defenses role, and was needed to protect coalition aircraft from Iraq's extensive air defense system. The RF-4C was the only aircraft equipped with the ultra-long-range KS-127 LOROP (long-range oblique photography) camera and was used for a variety of reconnaissance missions. In spite of flying almost daily missions, only one RF-4C was lost in a fatal accident before the start of hostilities. One F-4G was lost when enemy fire damaged the fuel tanks and the aircraft ran out of fuel near a friendly airbase. The last USAF Phantoms, F-4G Wild Weasel Vs from 561st Fighter Squadron, were retired on 26 March 1996. The last operational flight of the F-4G Wild Weasel was from the 190th Fighter Squadron, Idaho Air National Guard, in April 1996.[104] The last operational USAF/ANG F-4 to land was flown by Maj Mike Webb and Maj Gary Leeder of the Idaho ANG.[citation needed]
Target drone
[edit]Like the Navy, the Air Force also operated QF-4 target drones, serving with the 82d Aerial Targets Squadron at Tyndall Air Force Base, Florida, and Holloman Air Force Base, New Mexico.[105] Replacing the QF-106, the QF-4 program achieved IOC in 1997,[106] with the last QF-106 being shot down on 20 February 1997.[107] It was expected that the F-4 would remain in the target role with the 82d ATRS until at least 2015, when they would be replaced by early versions of the F-16 Fighting Falcon converted to a QF-16 configuration.[108]

On 19 November 2013, BAE Systems delivered its 314th, and last, QF-4 aerial target to the Air Force.[109] The example, RF-4C 68-0599, had been in storage for over 20 years before being converted.[110] Over 16 years, BAE had converted 314 F-4 and RF-4 Phantom IIs into QF-4s and QRF-4s, with each aircraft taking six months to adapt.[109] By December 2013, QF-4 and QRF-4 aircraft had flown over 16,000 manned and 600 unmanned training sorties, with 250 unmanned aircraft being shot down in firing exercises.[109] The remaining QF-4s and QRF-4s held their training role until the first of 126 QF-16s were delivered by Boeing.[109] The first QF-16 was delivered to Tyndall AFB in September 2014, achieving IOC on 23 September 2015.[111] The final flight of an Air Force QF-4 from Tyndall AFB took place on 27 May 2015 to Holloman AFB.[112]
After Tyndall AFB ceased operations, the 53d Weapons Evaluation Group at Holloman became the fleet of 22 QF-4s' last remaining operator. The base continued using them to fly manned test and unmanned live fire test support and Foreign Military Sales testing.[113] The final unmanned flight took place on 17 August 2016, with QF-4E 72-0166 being fired upon by a Lockheed Martin F-35 Lightning II before returning safely back to Holloman AFB.[114] The type was officially retired from US military service with a four–ship flight at Holloman during an event on 21 December 2016.[115] The last 13 QF-4s were stripped of their systems after 1 January 2017 and transferred to the White Sands Missile Range to be used as static targets.[111][116] During its career as a target drone, several QF-4s retained the capability to be flown as a manned aircraft and were maintained in historical color schemes, being displayed as part of Air Combat Command's Heritage Flight at air shows, base open houses, and other events while serving as non-expendable target aircraft during the week.[117]
Aerial combat in the Vietnam War
[edit]The USAF and the US Navy had high expectations of the F-4 Phantom, assuming that the massive firepower, the best available on-board radar, the highest speed and acceleration properties, coupled with new tactics, would provide Phantoms with an advantage over the MiGs. However, in confrontations with the lighter MiG-21, F-4s did not always succeed and began to suffer losses.[118] Over the course of the air war in Vietnam, between 3 April 1965 and 8 January 1973, each side would ultimately claim favorable kill ratios.[119]
During the war, U.S. Navy F-4 Phantoms claimed 40 air-to-air victories at a loss of seven Phantoms to enemy aircraft.[75] USMC F-4 pilots claimed three enemy MiGs at the cost of one aircraft in air-combat. USAF F-4 Phantom crews scored 107+1⁄2 MiG kills (including 33+1⁄2 MiG-17s, eight MiG-19s and 66 MiG-21s) at a cost of 33 Phantoms in air-combat.[94] F-4 pilots were credited with a total of 150+1⁄2 MiG kills at a cost of 42 Phantoms in air-combat.
According to the Vietnam People's Air Force (VPAF), 103 F-4 Phantoms were shot down by MiG-21s at a cost of 54 MiG-21s downed by F-4s.[120] During the war, the VPAF lost 131 MiGs in air combat (63 MiG-17s, eight MiG-19s and 60 MiG-21s) of which one half were by F-4s.[121]
From 1966 to November 1968, in 46 air battles conducted over North Vietnam between F-4s and MiG-21s, VPAF claimed 27 F-4s were shot down by MiG-21s at a cost of 20 MiG-21s[122] In 1970, one F-4 Phantom was shot down by a MiG-21.[123] The struggle culminated on 10 May 1972, with VPAF aircraft completing 64 sorties, resulting in 15 air battles. The VPAF claimed seven F-4s were shot down, while U.S. confirmed five F-4s were lost.[123] The Phantoms, in turn, managed to destroy two MiG-21s, three MiG-17s, and one MiG-19.[122] On 11 May, two MiG-21s, which played the role of "bait", brought the four F-4s to two MiG-21s circling at low altitude. The MiGs quickly engaged and shot down two F-4s. On 18 May, Vietnamese aircraft made 26 sorties in eight air engagements, which cost 4 F-4 Phantoms; Vietnamese fighters on that day did not suffer losses.[122]
On 5 August 1967, the USS Forrestal was stationed off the Indochina coast to carry out strikes against North Vietnam. An electrical fault caused a Zuni rocket to be fired from an F-4. The rocket struck the fuel tank of an A-4 Skyhawk attack aircraft, starting a fire which quickly spread to other airplanes, setting off several bombs. The fire and explosions killed 134 men and seriously wounded 161 more in what became known as the 1967 USS Forrestal fire.[124][125]
Non-U.S. users
[edit]The Phantom has served with the air forces of many countries, including Australia, Egypt, Germany, United Kingdom, Greece, Iran, Israel, Japan, Spain, South Korea and Turkey.
Australia
[edit]The Royal Australian Air Force (RAAF) leased 24 USAF F-4Es from 1970 to 1973 while waiting for their order for the General Dynamics F-111C to be delivered. They were so well-liked that the RAAF considered retaining the aircraft after the F-111Cs were delivered.[126] They were operated from RAAF Amberley by No. 1 Squadron and No. 6 Squadron.[127]
Egypt
[edit]In 1979, the Egyptian Air Force purchased 35 former USAF F-4Es along with a number of Sparrow, Sidewinder and Maverick missiles from the U.S. for $594 million as part of the "Peace Pharaoh" program.[128] An additional seven surplus USAF aircraft were purchased in 1988.[129] Three attrition replacements had been received by the end of the 1990s.[126]
Egyptian F-4Es were retired in 2020, with their former base at Cairo West Air Base being reconfigured for the operation of F-16C/D Fighting Falcons.[130]
Germany
[edit]The West German Air Force (Luftwaffe) found itself in need of numerous new aircraft following the December 1967 publication of NATO's new flexible response doctrine. With the move back towards fighting a conventional war in Europe, there was a need for both far more capable photoreconnaissance and fighter aircraft, with the RF-104G and F-104G fleets respectively being considered obsolescent due to their inability to operate in bad weather, at night, and in the latter's case, its performance being deemed insufficient for the air defense and air superiority missions against the MiG-21 that was fielded en masse by Warsaw Pact air forces. These new aircraft would need to enter service relatively quickly as well, with age and fatigue rates putting Luftwaffe strength below the required numbers by 1976. However, with the ongoing development of the Panavia Tornado there was insufficient capital to design new aircraft for these roles, and thus foreign models would have to be procured.[131]
Reconnaissance role
[edit]The photoreconnaissance aircraft selection pool was relatively small to start with, consisting of the Canadair CF-5A(R), Mirage IIIR, Saab S 35E, Lockheed RTF-104G, and McDonnell Douglas RF-4E. The competition came down to the RTF-104G and RF-4E, the former being a heavily modified phtoreconnaissance variant of the TF-104G and the latter an F-4E based equivalent to the USAF's own RF-4C intended for export customers. As the RTF-104G could still reuse most existing infrastructure at bases operating RF-104Gs while RF-4Es could not, the latter had a substantially higher unit price - 23 million Deutsche Marks for an RF-4E compared to 8 million DM for an RTF-104G. The latter was also considered slightly more modern, and could be built under license on the existing F-104G production line at Messerschmitt-Bölkow-Blohm (MBB), meaning most of the money would be kept in West Germany. However, the safety and power advantages of the Phantom were viewed very favorably - the USAF had experienced loss rates of 9 F-4 versus 25 F-104 for every 100,000 flight hours, and West German experience with the F-104 platform was marred with crashes. Another factor in the Phantom's favor was industrial offsets, as West Germany had set aside 3 billion DM to purchase defense equipment from the U.S.[132] which could be used outside of the normal defense budget to fund this acquisition. In 1969, the German Defense Ministry decided to procure 88 RF-4Es, with the contract costing 2.052 billion DM. While not manufactured in West Germany, their construction was not wholly American. Companies like MBB produced stabilizers, landing gear doors, outer wings, and ailerons which were then shipped to McDonnell Douglas's St. Louis factory for final assembly.[133]
The RF-4E first flew on 15 September 1970, and the West Germans took delivery of their first four aircraft at Bremgarten AB on 20 January 1971.[134] To act as flight instructors, nine pilots and nine navigators were sent to Shaw AFB between 22 January 1970 and 5 May 1971 to attend eight to nine month long training courses on the RF-4C. 108 pilots were trained at George AFB between 10 October 1970 and 4 February 1972 for five week flight training courses. These pilots had to receive sensor training from the aforementioned flight instructors after returning to their units in West Germany.[135]
With the lethality of Warsaw Pact air defenses increasing along with the strength of their conventional ground forces over the course of the 1970s, in 1978 it was decided to simultaneously retrofit the aircraft for a secondary ground attack role using the same equipment as the F-4F, and to improve their self-defense capabilities by fitting improved flare and chaff systems and a more capable radar warning receiver. New infrared cameras were also fitted for improved reconnaissance capabilities.[136] 71 aircraft were again upgraded in the mid 1980's, as planners saw no replacement for the type available before 2005. These included an increase in maximum flight hours for 4,500 to 8,000 per airframe, the installation of a laser and GPS navigation system, a new AN/APQ-172 terrain following radar, and integration for the new AIM-9L Sidewinder.[137] However, after German reunification and the end of the Cold War, there was a sharp drawdown in military spending.[138] 27 RF-4Es were sold to the Greek Air Force, of which seven were spares. Another 46 were sold to the Turkish Air Force - 33 operational aircraft and 13 spares.[139] The Luftwaffe retired the type in 1994,[140] and the last example was handed over to the Museum of the Luftwaffe on 23 November 2003.[141]
Fighter role
[edit]The fighter contract was designed to prevent the loss rates that had plagued F-104 in Luftwaffe service from repeating. Two of the key requirements in the new fighter program were an all-weather navigation system and two engines. The competition also featured a greater variety of contestants, with the SEPECAT Jaguar, Saab Viggen, Dassault Mirage F1, Northrop F-5, Northrop P-530, and McDonnell Douglas F-4F all being offered. With RF-4E already being adopted, combined with F-4F's advantages in range and weapons load, it was the declared the winner and an order for 175 aircraft placed on 24 June 1971 under the "Peace Rhine" program, with a unit price of approximately 12 million DM. The “F” variant was a simplified version of the “E”, designed for maximum compatibility with RF-4E. The aircraft was roughly 1,500 kilograms (3,300 lb) lighter, lacking the ram air turbine, rear fuselage fuel tank, slatted stabilizers, and ability to use AIM-7 Sparrow.[142] However, these weight reductions combined with the leading edge slats that were not present on RF-4E made F-4F markedly more maneuverable, especially at low speeds. All but the first F-4F incorporated West German built subcomponents in the same manner as their RF-4Es.[143] All F-4Fs were delivered between 1973 and 1976.[144] These purchases made Germany the largest export customer for the Phantom.[145]
The F-4F first flew on 18 March 1973, and was publicly unveiled on 24 May of the same year. Shortly thereafter, the first 12 aircraft were delivered to George AFB in cooperation with the 35th Tactical Fighter Wing to stand up an operational conversion unit, with pilots of Jagdgeschwader 71 (Fighter Wing 71) arriving on 1 January 1974 to begin training. Due to the urgent need for the aircraft in frontline service, West Germany replaced these F-4Fs with 10 new F-4Es in 1975, which were permanently stationed in the U.S. for training until their retirement in 1997.[146] A single F-4F was kept in the U.S. on loan to U.S. Air Force Systems Command until 1982 under the designation NTF-4F, which was used as a testbed for new technologies in the aircraft.[147] The F-4F was upgraded in the mid-1980s[148] to use more capable ordnance that was being introduced by the U.S. in light of new capabilities introduced by the Warsaw Pact militaries. These alterations included a new digital weapons computer, altering the radar to allow for bombing through cloud cover, a HUD, and integration of the AIM-9L Sidewinder and AGM-65B Maverick.[149] The droptank was replaced with a lower drag model used by F-15C, and both the radar warning receiver and jamming pods were upgraded. The chaff/flare dispensers were also replaced with more capable models.[150]
Much as the Warsaw Pact's improving conventional strengths had seen a need for a more capable reconnaissance aircraft, the increasing lethality of air defenses and aircraft saw a similar need for more capable fighters. While procurement of the Tornado ADV was considered, it was decided against in favor of upgrading the F-4F fleet. The program, known as Improved Combat Efficiency (ICE) or Kampfwertsteigerung (KWS) began in 1983 and sought to fit the aircraft with substantially improved air to air and air to ground weapons, including beyond-visual-range missiles and standoff weapons[151] To start, the 153 F-4Fs in frontline service all received modest upgrades known as KWS-LA (ground attack, luftangriff), including a laser navigation system and structural upgrades to extend maximum flight hours from 4,000 to 6,500 per airframe. 110 of these were further upgraded under KWS-LV (air defense, luftverteidigung) with the AN/APG-65GY radar, a new mission computer, and compatibility with AIM-120 AMRAAM.[152] The KWS-LV F-4Fs entered service in 1992,[148] and were expected to remain in service until 2012.[153] All the remaining Luftwaffe Phantoms were based at Wittmund with Jagdgeschwader 71 in Northern Germany[154] and WTD61 at Manching. A total of 24 F-4Fs were operated by the 49th Tactical Fighter Wing of the USAF at Holloman AFB to train Luftwaffe crews until December 2004. Phantoms were deployed to NATO states under the Baltic Air Policing starting in 2005, 2008, 2009, 2011 and 2012. The German Air Force retired its last F-4Fs on 29 June 2013. German F-4Fs flew 279,000 hours from entering service on 31 August 1973 until retirement.[155][156]
Greece
[edit]In 1972, the Hellenic Air Force signed a contract for 36 brand new F-4E Phantoms, with deliveries starting in 1974.[157][158][159] In the early 1990s, the Hellenic AF acquired surplus RF-4Es and F-4Es from the Luftwaffe and U.S. ANG.[160][161] Following the success of the German ICE program, on 11 August 1997, a contract was signed between DASA of Germany and Hellenic Aerospace Industry for the upgrade of 39 aircraft to the very similar "Peace Icarus 2000" standard.[26] On 5 May 2017, the Hellenic Air Force officially retired the RF-4E Phantom II during a public ceremony.[162]
Iran
[edit]
In the 1960s and 1970s when the U.S. and Iran were on friendly terms, the U.S. delivered 225 F-4D, F-4E, and RF-4E Phantoms to Iran, making it the second largest export customer.[163] The Imperial Iranian Air Force saw at least one engagement, resulting in a loss, after an RF-4C was rammed[164] by a Soviet MiG-21 during Project Dark Gene, an ELINT operation during the Cold War.
The Islamic Republic of Iran Air Force Phantoms saw heavy action in the Iran–Iraq War in the 1980s and were kept operational by overhaul and servicing from Iran's aerospace industry.[165] Notable operations of Iranian F-4s during the war included Operation Scorch Sword, an attack by two F-4s against the Iraqi Osirak nuclear reactor site near Baghdad on 30 September 1980,[166] and the attack on H3, a 4 April 1981 strike by eight Iranian F-4s against the H-3 complex of air bases in the far west of Iraq, which resulted in many Iraqi aircraft being destroyed or damaged for no Iranian losses.[167]
On 5 June 1984, two Saudi Arabian fighter pilots shot down two Iranian F-4 fighters. The Royal Saudi Air Force pilots were flying American-built F-15s and fired air-to-air missiles to bring down the Iranian planes. The Saudi fighter pilots had Boeing KC-135 Stratotanker planes and Boeing E-3 Sentry AWACS surveillance planes assist in the encounter. The aerial fight occurred in Saudi airspace over the Persian Gulf near the Saudi island Al Arabiyah, about 60 miles northeast of Jubail.[168]
Iranian F-4s were in use as of late 2014;[169] the aircraft reportedly conducted air strikes on ISIS targets in the eastern Iraqi province of Diyala.[170]
At the 2024 Kish Air Show, three F-4Es from the 91st Tactical Combat Squadron, operating out of their home base in Bandar Abbas, performed formation and solo flyovers.[171]
Israel
[edit]
The Israeli Air Force acquired between 212 and 222[172] newly built and ex-USAF aircraft, and modified several as one-off special reconnaissance variants. The first F-4Es, nicknamed "Kurnass" (Sledgehammer), and RF-4Es, nicknamed "Orev" (Raven), were delivered in 1969 under the "Peace Echo I" program. Additional Phantoms arrived during the 1970s under "Peace Echo II" through "Peace Echo V" and "Nickel Grass" programs. Israeli Phantoms saw extensive combat during Arab–Israeli conflicts, first seeing action during the War of Attrition.[173] In the 1980s, Israel began the "Kurnass 2000" modernization program which significantly updated avionics.[26] The last Israeli F-4s were retired in 2004.[174]
Japan
[edit]From 1968, the Japan Air Self-Defense Force (JASDF) purchased a total of 140 F-4EJ Phantoms without aerial refueling, AGM-12 Bullpup missile system, nuclear control system or ground attack capabilities.[175][176] Mitsubishi built 138 under license in Japan and 14 unarmed reconnaissance RF-4Es were imported. One of the aircraft (17-8440) was the last of the 5,195 F-4 Phantoms to be produced. It was manufactured by Mitsubishi Heavy Industries on 21 May 1981. "The Final Phantom" served with 306th Tactical Fighter Squadron and later transferred to the 301st Tactical Fighter Squadron.[citation needed]

Of these, 96 F-4EJs were modified to the F-4EJ Kai (改; modified) standard.[177] 15 F-4EJ and F-4EJ Kai were converted to reconnaissance aircraft designated RF-4EJ. Japan had a fleet of 90 F-4s in service in 2007. After studying several replacement fighters[178][179] the F-35A Lightning II was chosen in 2011.[180] The 302nd Tactical Fighter Squadron became the first JASDF F-35 Squadron at Misawa Air Base when it converted from the F-4EJ Kai on 29 March 2019.[181] The JASDF's sole aerial reconnaissance unit, the 501st Tactical Reconnaissance Squadron, retired their RF-4Es and RF-4EJs on 9 March 2020, and the unit itself dissolved on 26 March.[182]
The 301st Tactical Fighter Squadron then became the sole user of the F-4EJ in the Air Defense Command, with their retirement originally scheduled in 2021 along with the unit's transition to the F-35A.[183] However, on 20 November 2020, the 301st Tactical Fighter Squadron announced the earlier retirement of their remaining F-4EJs, concluding the Phantom's long-running career in the JASDF Air Defense Command.[184] Although retirement was announced, the 301st TFS continued operations up until 10 December 2020, with the squadron's Phantoms being decommissioned on 14 December.[185] Two F-4EJs and a F-4EJ Kai continued to be operated by the Air Development and Test Wing in Gifu Prefecture until their retirement on 17 March 2021, marking an end of Phantom operations in Japan.[2]
South Korea
[edit]The Republic of Korea Air Force received its first batch of used USAF F-4D Phantoms in 1969 under the "Peace Spectator" program. The F-4Ds continued to be delivered until 1988. The "Peace Pheasant II" program also provided new-built and former USAF F-4Es.[186] In 1975, South Korea fundraised to buy five new F-4 Phantoms with the money donated from South Korean citizens in a national fundraising drive set up to buy the jets (a necessity at the time as South Korea was a poor country and in the aftermath of the Korean War, needed the extra jets to defend against North Korea which had a larger air force back then).[187] In total, the ROKAF operated 92 F-4Ds, 27 RF-4Cs, and 103 F-4Es.[188] The last ROKAF F-4Es were retired on 7 June 2024.[3]
Spain
[edit]The Spanish Air Force acquired its first batch of ex-USAF F-4C Phantoms in 1971 under the "Peace Alfa" program. Designated C.12, the aircraft were retired in 1989. At the same time, the air arm received a number of ex-USAF RF-4Cs, designated CR.12. In 1995–1996, these aircraft received extensive avionics upgrades. Spain retired its RF-4s in 2002.[189][190]
Turkey
[edit]
The Turkish Air Force (TAF) received 40 F-4Es in 1974, with a further 32 F-4Es and 8 RF-4Es in 1977–78 under the "Peace Diamond III" program, followed by 40 ex-USAF aircraft in "Peace Diamond IV" in 1987, and a further 40 ex-U.S. Air National Guard Aircraft in 1991.[191] A further 32 RF-4Es were transferred to Turkey after being retired by the Luftwaffe between 1992 and 1994.[191] In 1995, Israel Aerospace Industries (IAI) implemented an upgrade similar to Kurnass 2000 on 54 Turkish F-4Es which were dubbed the F-4E 2020 Terminator.[26] Turkish F-4s, and more modern F-16s have been used to strike Kurdish PKK bases in ongoing military operations in Northern Iraq.[192] On 22 June 2012, a Turkish RF-4E was shot down by Syrian air defenses while flying a reconnaissance flight near the Turkish-Syrian border.[193][194] Turkey has stated the reconnaissance aircraft was in international airspace when it was shot down, while Syrian authorities stated it was inside Syrian airspace.[195] Turkish F-4s remained in use as of 2020,[169][196] and it plans to fly them at least until 2030.[197]

On 24 February 2015, two RF-4Es crashed in the Malatya region in southeastern Turkey under unknown circumstances, killing both crewmembers of each aircraft.[198][199][200] On 5 March 2015, an F-4E-2020 crashed in central Anatolia killing both crew.[201][202] After the recent accidents, the TAF withdrew RF-4Es from active service. Turkey was reported to have used F-4 jets to attack PKK separatists and the ISIS capital on 19 September 2015.[203] The Turkish Air Force has reportedly used the F-4E 2020s against the more recent Third Phase of the PKK conflict on heavy bombardment missions into Iraq on 15 November 2015, 12 January 2016, and 12 March 2016.[204][205]
United Kingdom
[edit]
The United Kingdom bought versions based on the U.S. Navy's F-4J for use with the Royal Air Force and the Royal Navy's Fleet Air Arm. The UK was the only country outside the United States to operate the Phantom at sea, with them operating from HMS Ark Royal. The main differences were the use of the British Rolls-Royce Spey engines and of British-made avionics. The RN and RAF versions were given the designation F-4K and F-4M respectively, and entered service with the British military aircraft designations Phantom FG.1 (fighter/ground attack) and Phantom FGR.2 (fighter/ground attack/reconnaissance).[206][207]
Initially, the FGR.2 was used in the ground attack and reconnaissance role, primarily with RAF Germany, while 43 Squadron was formed in the air defense role using the FG.1s that had been intended for the Fleet Air Arm for use aboard HMS Eagle. The superiority of the Phantom over the English Electric Lightning in terms of both range and weapons system capability, combined with the successful introduction of the SEPECAT Jaguar, meant that, during the mid-1970s, most of the ground attack Phantoms in Germany were redeployed to the UK to replace air defense Lightning squadrons.[208] A second RAF squadron, 111 Squadron, was formed on the FG.1 in 1979 after the disbandment of 892 NAS.
In 1982, during the Falklands War, three Phantom FGR2s of No. 29 Squadron were on active Quick Reaction Alert duty on Ascension Island to protect the base from air attack.[209] After the Falklands War, 15 upgraded ex-USN F-4Js, known as the F-4J(UK) entered RAF service to compensate for one interceptor squadron redeployed to the Falklands.[148]
Around 15 RAF squadrons received various marks of Phantom, many of them based in Germany. The first to be equipped was No. 228 Operational Conversion Unit at RAF Coningsby in August 1968. One noteworthy operator was No. 43 Squadron where Phantom FG1s remained the squadron equipment for 20 years, arriving in September 1969 and departing in July 1989. During this period the squadron was based at Leuchars.[210]
The interceptor Phantoms were replaced by the Panavia Tornado F3 from the late 1980s onwards. Originally to be used until 2003,[211] it was set back to 1992 due to restructuring of the British Armed Forces[212] and the last combat British Phantoms were retired in October 1992 when No. 74(F) Squadron was disbanded.[26][210] Phantom FG.1 XT597 was the last British Phantom to be retired on 28 January 1994, it was used as a test jet by the Aeroplane and Armament Experimental Establishment for its whole service life.[213][214]
Civilian use
[edit]In 1988, Sandia National Laboratories mounted an F-4 on a "rocket sled", then crashed it into reinforced concrete to learn about the collision of aircraft with structures such as a nuclear power plant.[215]

An F-4D (civilian registration NX749CF) is operated by the Massachusetts-based non-profit organization Collings Foundation as a "living history" exhibit.[26][216] Funds to maintain and operate the aircraft, which is based in Houston, Texas, are raised through donations and sponsorships from public and commercial parties.[217][218]
In the 1960s, NASA used the F-4 to photograph and film Titan II missiles after their launch from Cape Canaveral after finding the Lockheed F-104 Starfighter inadequate. Jack Petry, a retired U.S. Air Force colonel, said he put his F-4 into a Mach 1.2 dive synchronized to the launch countdown, then "walked the [rocket's] contrail". Petry's Phantom stayed with the Titan for 90 seconds, reaching 68,000 feet, then broke away as the missile continued into space.[24]
NASA's Flight Research Center acquired an F-4A on 3 December 1965. It made 55 flights flying chase on X-15 missions and lifting body flights. The F-4 also supported a biomedical monitoring program involving 1,000 flights by NASA Flight Research Center aerospace research pilots and students of the USAF Aerospace Research Pilot School flying high-performance aircraft. The pilots were instrumented to record accurate and reliable data of electrocardiogram, respiration rate, and normal acceleration. In 1967, the Phantom supported a brief military-inspired program to determine whether an airplane's sonic boom could be directed and whether it could be used as a weapon of sorts, or at least an annoyance. NASA also flew an F-4C in a spanwise blowing study from 1983 to 1985, after which it was returned.[219]
Culture
[edit]Legacy
[edit]The F-4 Phantom II is widely regarded as an iconic aircraft of post-WWII military aviation, celebrated for its versatility, performance, and distinctive design. With its bold lines and commanding presence, the Phantom earned deep respect for its performance, adaptability, and symbolic weight across generations of pilots and enthusiasts. Its long service life and widespread use in multiple roles have cemented its status as a symbol of military aviation.[220] With 5,195 Phantom II aircraft produced over more than 20 years in multiple variants, the F-4 achieved huge commercial success as the best-selling supersonic fighter in U.S. history.[221] It currently remains the latest, and final aircraft model to produce "ace-status" for a member of any branch of the United States armed forces.
Nicknames
[edit]
The Phantom gathered a number of nicknames during its career. Some of these names included "Snoopy", "Rhino", "Double Ugly",[222] "Old Smokey",[87] the "Flying Anvil", "Flying Footlocker", "Flying Brick", "Lead Sled", the "Big Iron Sled", and the "St. Louis Slugger" (owing to it being produced in St. Louis).[223] In recognition of its record of downing large numbers of Soviet-built MiGs,[224] it was called the "World's Leading Distributor of MiG Parts".[222] As a reflection of excellent performance in spite of its bulk, the F-4 was dubbed "the triumph of thrust over aerodynamics."[225] German Luftwaffe crews called their F-4s the Eisenschwein ("Iron Pig"), Fliegender Ziegelstein ("Flying Brick") and Luftverteidigungsdiesel ("Air Defense Diesel").[226] In the RAF it was most commonly referred to as "The Toom" (not tomb).[227] Whilst the Turkish Air Force crewmen nicknamed it as Baba ("Father").[228]
Reputation
[edit]Imitating the spelling of the aircraft's name, McDonnell issued a series of patches. Pilots became "Phantom Phlyers", backseaters became "Phantom Pherrets", fans of the F-4 "Phantom Phanatics", and call it the "Phabulous Phantom". Ground crewmen who worked on the aircraft are known as "Phantom Phixers".[6]
Several active websites are devoted to sharing information on the F-4, and the aircraft is grudgingly admired as brutally effective by those who have flown it. Colonel (Ret.) Chuck DeBellevue reminisced, "The F-4 Phantom was the last plane that looked like it was made to kill somebody. It was a beast. It could go through a flock of birds and kick out barbeque from the back."[229] It had "A reputation of being a clumsy bruiser reliant on brute engine power and obsolete weapons technology."[230]
The Spook
[edit]
The aircraft's emblem is a whimsical cartoon ghost called "The Spook", which was created by McDonnell Douglas technical artist, Anthony "Tony" Wong, for shoulder patches. The name "Spook" was coined by the crews of either the 12th Tactical Fighter Wing or the 4453rd Combat Crew Training Wing at MacDill AFB. The figure is ubiquitous, appearing on many items associated with the F-4. The Spook has followed the Phantom around the world adopting local fashions; for example, the British adaptation of the U.S. "Phantom Man"[222] is a Spook that sometimes wears a bowler hat and smokes a pipe.[231]
Variants
[edit]
- F-4A, B, J, N and S
- Variants for the U.S. Navy and the U.S. Marine Corps. F-4B was upgraded to F-4N, and F-4J was upgraded to F-4S.
- F-110 (original USAF designation for F-4C), 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 produced, 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 Suppression of Enemy Air Defenses (SEAD) variant for the U.S. Air Force with updated radar and avionics, converted from F-4E. The designation F-4G was applied earlier to an entirely different U.S. Navy Phantom.
- F-4K and M
- Variants for the Royal Navy and Royal Air Force, respectively, built with Rolls-Royce Spey turbofan engines.
- F-4EJ and RF-4EJ
- Simplified F-4E exported to and license-built in Japan. Some modified for reconnaissance role, carrying photographic or electronic reconnaissance pods and designated RF-4EJ.
- F-4F
- Simplified F-4E exported to Germany.
- QRF-4C, QF-4B, E, G, N and S
- Retired aircraft converted into remote-controlled target drones used for weapons and defensive systems research by USAF and USN / USMC.
- RF-4B, C, and E
- Tactical reconnaissance variants.
Operators
[edit]
Current
[edit]
- Hellenic Air Force – 17 F-4E AUPs (Peace Icarus 2000 variant) in service as of 2024[232][233][234]
- Islamic Republic of Iran Air Force – 62 F-4D, F-4E, and RF-4Es in service as of 2021[232][235]
- Bandar Abbas Air Base, Hormozgan Province
- 91st Tactical Fighter Squadron (F-4E)
- Bushehr Air Base, Bushehr Province
- 61st Tactical Fighter Squadron (F-4E)
- Chabahar Konarak Air Base, Sistan and Baluchestan Province
- 101st Tactical Fighter Squadron (F-4D)
- Hamadan Air Base, Hamadan Province
- 31st Tactical Reconnaissance Squadron (RF-4E)
- 31st Tactical Fighter Squadron (F-4E)
- Bandar Abbas Air Base, Hormozgan Province

- Turkish Air Force – 19 F-4E 2020 Terminators in service as of 2024[236]
- Eskişehir Air Base, Eskişehir Province
- 111 Filo
- Eskişehir Air Base, Eskişehir Province
Former operators
[edit]
- Royal Australian Air Force (F-4E 1970 to 1973)[237]
- Egyptian Air Force (F-4E 1977 to 2020)[130]
- German Air Force (RF-4E 1971 to 1994; F-4F 1973 to 2013; F-4E 1978 to 1992)[238]
- Hellenic Air Force (RF-4E 1978 to 2017)[162]
- Israeli Air Force (F-4E 1969 to 2004;[239] RF-4C 1970 to 1971;[240] RF-4E 1971 to 2004)[241]
- Japan Air Self-Defense Force (F-4EJ 1971 to 2021;[2] RF-4E 1974 to 2020; RF-4EJ 1992 to 2020)[242]
- Republic of Korea Air Force (F-4D 1969 to 2010;[243] RF-4C 1989 to 2014;[244] F-4E 1977 to 2024)

- Spanish Air Force (F-4C 1971 to 1990; RF-4C 1978 to 2002)[245]
- Turkish Air Force (RF-4E 1980 to 2015)[246]
- Aeroplane and Armament Experimental Establishment (F-4K 1970 to 1994)[247]
- Fleet Air Arm (F-4K 1968 to 1978)[208]
- Royal Air Force (F-4M 1968 to 1992; F-4K 1969 to 1990; F-4J(UK) 1984 to 1991)[208]
- NASA (F-4A 1965 to 1967;[248] F-4C 1983 to 1985)[219]
- United States Air Force (F-4B 1963 to 1964;[249] F-4C 1964 to 1989;[250] RF-4C 1964 to 1995;[251] F-4D 1965 to 1992; F-4E 1967 to 1991;[250] F-4G 1978 to 1996;[249] QF-4 1997 to 2016)[252][1]
- United States Marine Corps (F-4B 1962 to 1979; RF-4B 1965 to 1990; F-4J 1967 to 1984;[253] F-4N 1973 to 1985;[254] F-4S 1978 to 1992)[253]
- United States Navy (F-4A 1960 to 1968; F-4B 1961 to 1974; F-4J 1966 to 1982; F-4N 1973 to 1984; F-4S 1979 to 1987; QF-4 1983 to 2004)[255]
Privately owned
[edit]- Platinum Fighters Sale – 1 F4H-1F[256]
Notable accidents
[edit]- On 6 June 1971, Hughes Airwest Flight 706, a McDonnell Douglas DC-9-31 collided in mid-air with a United States Marine Corps F-4B Phantom above the San Gabriel Mountains, while en route from Los Angeles International Airport to Salt Lake City. All 49 on board the DC-9 were killed, while the pilot of the F-4B was unable to eject and died when the aircraft crashed shortly afterwards. The F-4B's Radar Intercept Officer successfully ejected from the plane and parachuted to safety, being the sole survivor of the incident.
- On 9 August 1974, a Royal Air Force Phantom FGR2 was involved in a fatal collision with a civilian PA-25-235 Pawnee crop-sprayer over Norfolk, England.[257]
- On 1 October 1976, an RF-4C Phantom II impacted terrain on Holston Mountain near the Holston Mountain VORTAC, just north of Elizabethton, TN. Both crew members were killed.[258]
- On 17 August 1978, during a training exercise over the Mediterranean Sea, a US Navy F-4 shot down another US Navy F-4 with an AIM-9H. The pilots of the downed aircraft ejected and were recovered.[259]
- On 21 March 1987, Captain Dean Paul Martin, a pilot in the 163d Tactical Fighter Group of the California Air National Guard and son of entertainer Dean Martin, crashed his F-4C into San Gorgonio Mountain, California, shortly after departure from March Air Force Base. Both Martin and his weapon systems officer (WSO) were killed.[260]
- On 22 September 1987, a US Air Force RF-4C Phantom II was shot down by a US Navy F-14 Tomcat during training NATO Exercise Display Determination 87 over the Mediterranean. The RF-4C was conducting a simulated attack on USS Saratoga when the F-14 pilot became confused and launched a live AIM-9 Sidewinder. The RF-4C crew ejected and were recovered.[261][262]
- On 30 January 2023, a Greek Air Force F-4E Phantom II crashed into the Ionian Sea. The aircraft was conducting a training exercise when it crashed 46 km south of the Andravida Air Base. The pilot and co-pilot were killed in the crash.[263][264]
Aircraft on display
[edit]As a result of its extensive number of operators and large number of aircraft produced, a significant number of F-4 Phantom IIs of a variety of variants have been preserved in museums and other locations around the world.
Gallery
[edit]-
Structural view of partially disassembled German F-4 Phantoms (2009).
-
VF-96 F-4J "Showtime 100" armed with Sidewinder and Sparrow missiles (1972).
-
A Republic of Korea Air Force F-4D Phantom II armed with AIM-9 missiles at Daegu Air Base, 1979.
Video resources
[edit]-
"The Record Breaking Phantom II" Mcdonnell aircraft promotional Film.
-
"The F-4 Phantom Joins the Fleet" (1962).
-
F-4J Phantom II AWG-10 guided missile trials at Pt. Mugu, California.
-
"Ambassadors in Blue" (1971) F-4E Phantom USAF Thunderbirds promotional film.
-
USAF F-4 Phantom II conventional weapons delivery dive-bombing training film.
-
USAF tactical weapons in South-East Asia.
Specifications (F-4E)
[edit]Data from The Great Book of Fighters,[148] Quest for Performance,[25] Encyclopedia of USAF Aircraft,[67] and McDonnell F-4 Phantom: Spirit in the Skies[265]
General characteristics
- Crew: 2
- Length: 63 ft 0 in (19.2 m)
- Wingspan: 38 ft 5 in (11.7 m)
- Width: 27 ft 7 in (8.4[266] m) wing folded
- Height: 16 ft 5 in (5 m)
- Wing area: 530 sq ft (49.2 m2)
- Aspect ratio: 2.77
- Airfoil: NACA 0006.4–64 root, NACA 0003-64 tip
- 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) or 12,961 lb (5,879 kg) internal, 3,335 US gal (2,777 imp gal; 12,620 L) or 21,678 lb (9,833 kg) 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)
Armament
- E-model has a 20 mm (0.787 in) M61A1 Vulcan cannon mounted internally under the nose, 640 rounds
- 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, 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-3.
- 4× AIM-7 Sparrow in fuselage recesses, upgraded Hellenic F-4E and German F-4F ICE carry AIM-120 AMRAAM, UK Phantoms carried Skyflash missiles[267]
- 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
- 18× CBU-87, CBU-89, CBU-58
- 12x MK-20 Rockeye
- Nuclear weapons, including the B28EX, B61, B43 and B57
Avionics
- AN/APG-30 – fire-control radar
- AN/APG-76 – Multimode synthetic-aperture radar
- AN/APQ-117 – Terrain-following radar
- AN/ASQ-153 – Part of Pave Spike laser designator targeting pod
- AN/ASX-1 – Target Identification System Electro-Optical (TISEO)
- AN/AVQ-23 – Part of Pave Spike laser designator targeting pod
See also
[edit]Related development
Aircraft of comparable role, configuration, and era
- Dassault Mirage III
- English Electric Lightning
- Mikoyan-Gurevich MiG-21
- Mikoyan-Gurevich MiG-23
- Republic F-105 Thunderchief
- Saab 35 Draken
- Shenyang J-8
- Sukhoi Su-15
- Vought XF8U-3 Crusader III
Related lists
References
[edit]Notes
[edit]- ^ The aircraft was originally designated the AH, and later re-designated F4H, by the United States Navy, while the U.S. Air Force's original designation was "F-110A Spectre". The F-4 designation came about in the 1962 United States Tri-Service aircraft designation system for all branches of the U.S. military, unified by the order of U.S. Defense Secretary Robert McNamara. Within McDonnell Aircraft, the F-4 was referred to as Model 98.[4]
Citations
[edit]- ^ a b Devine, Jacqueline. "USAF bids farewell to F-4 Phantom". Military 1. Archived from the original on 7 February 2017. Retrieved 6 February 2017.
- ^ a b c Cenciotti, David (17 March 2021). "Japan's Last Three F-4EJ Phantoms Have Just Flown For The Last Time". The Aviationist. Archived from the original on 18 March 2021. Retrieved 17 March 2021.
- ^ a b Kim, Hyun-Bin (7 June 2024). "South Korea bids farewell to legendary F-4 Phantom fighter jet". The Korea Times. Retrieved 7 June 2024.
- ^ "Boeing: Historical Snapshot: F-4 Phantom II Fighter". boeing.com. Archived from the original on 14 August 2020. Retrieved 29 August 2020.
- ^ a b c d e f "F-4 Phantoms Phabulous 40th". Boeing. Retrieved : 27 November 2012.
- ^ "First to Last", Phabulous 40th, Boeing, archived from the original on 13 December 2009, retrieved 19 November 2007.
- ^ Wragg, David W. (1973). A Dictionary of Aviation (first ed.). Osprey. p. 122. ISBN 9780850451634.
- ^ a b "Phantom 'Phirsts'", Phabulous 40th, Boeing, archived from the original on 29 June 2011, retrieved 27 November 2012.
- ^ a b c d e f g h "World Record Holder", Phabulous 40th, Boeing, archived from the original on 6 July 2009, retrieved 14 December 2007.
- ^ a b c Dorr and Bishop 1996, pp. 200–201.
- ^ a b Dorr and Bishop 1996, pp. 188–189.
- ^ Donald Spring 1991, p. 26.
- ^ Donald Summer 1991, p. 22.
- ^ a b Lake 1992, p. 190.
- ^ Lake 1992, p. 203.
- ^ "Equipment - Hellenic Air Force". Hellenic Air Force (in Greek). Archived from the original on 20 March 2025. Retrieved 28 June 2025.
- ^ Iddon, Paul. "F-4 Drop Tank Incident Underscores Turkey's Need To Replace Its Aging Phantom Fleet". Forbes. Retrieved 10 July 2025.
- ^ Thornborough and Davies 1994, p. 13.
- ^ Thornborough and Davies 1994, p. 11.
- ^ Dorr 2008, p. 61.
- ^ "Phabulous 40th: Phantom Development." Archived 7 September 2009 at the Wayback Machine 1978 Commemorative Book. Boeing. Retrieved: 14 February 2008.
- ^ Lake 1992, p. 15.
- ^ a b c d e f g h i j Joiner, Stephen (March 2015). "What Couldn't the F-4 Phantom Do?". Air & Space. Archived from the original on 6 June 2020. Retrieved 5 June 2020.
- ^ a b c Loftin, Laurence K. Quest for Performance: The Evolution of Modern Aircraft SP-468. Archived 13 June 2006 at the Wayback Machine Washington, DC: National Aeronautics and Space Administration, History Office, Scientific and Technical Information Branch, 1985. Retrieved: 19 November 2007.
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- ^ "This day in aviation: 6 December 1959" Archived 26 April 2014 at the Wayback Machine Bryan R. Swopes. Retrieved: 25 April 2014.
- ^ Lake 1992, pp. 16, 17.
- ^ “Naval Aviation News”, July 1961, p. 6
- ^ Stein, Alan J. "Seattle native Dick Gordon orbits the moon on 18 November 1969." Archived 30 May 2008 at the Wayback Machine HistoryLink.org, 13 June 1999. Retrieved: 13 February 2008.
- ^ Grossnick, Roy A. "Part 9 – The Sixth Decade 1960–1969." Archived 27 February 2008 at the Wayback Machine history.navy.mil. Retrieved: 21 July 2010.
- ^ "United States Naval Aviation 1910–1995." Archived 12 September 2012 at the Wayback Machine Naval Historical Center, 1997. Retrieved: 21 July 2010.
- ^ "McDonnell F-4A (F4H-1) Phantom II 'Sageburner'." National Air and Space Museum, Smithsonian Institution. Retrieved: 22 August 2011.
- ^ McComb, Enterprise Journal, USM.
- ^ "22 November 1961". This Day in Aviation. 22 November 2016. Archived from the original on 15 March 2017. Retrieved 15 March 2017.
- ^ "22 November 1961". 22 November 2021. Archived from the original on 15 March 2017. Retrieved 15 March 2017.
- ^ Thornborough and Davies 1994, p. 15.
- ^ "Naval Aviation News", April 1962, p. 12
- ^ "Naval Aviation News", June 1962, p. 12
- ^ "USN Photo 1143454". Archived from the original on 7 May 2022. Retrieved 7 May 2022.
- ^ "US Navy and US Marine Corps BuNos--Third Series (145062 to 150138)". www.joebaugher.com. Archived from the original on 17 June 2010. Retrieved 7 May 2022.
- ^ “Naval Aviation News”, April 1962, p. 12
- ^ ”Naval Aviation News”, June 1962, p. 12
- ^ "Phabulous 40th: Current Uses of Titanium: F-4." Archived 9 September 2009 at the Wayback Machine Boeing, 1971. "F-4B/C 1,006 lb. 7.7% of Structure, F-J/E 1,261 lb. 8.5% of Structure". Retrieved: 14 February 2008.
- ^ Donald and Lake 1996, p. 268.
- ^ Dorr and Donald 1990, p. 198.
- ^ McDonnell Douglas F-4D "Phantom II". Archived 23 September 2009 at the Wayback Machine National Museum of the USAF. Retrieved: 20 January 2008.
- ^ Angelucci 1987, p. 310.
- ^ Donald, David. Warplanes of the Fleet. London: AIRtime Publishing Inc., 2004. ISBN 1-880588-81-1.
- ^ Goebel, Greg. "Phantom Over Southeast Asia." Vectorsite.net. Retrieved: 18 January 2008.
- ^ a b Higham and Williams 1978.
- ^ "McDonnell Douglas F-4S Phantom" Archived 27 February 2010 at the Wayback Machine MAPS Air Museum at Akron-Canton Airport. Retrieved: 28 March 2010.
- ^ Richardson and Spick 1984, p. 25.
- ^ a b c Knaack 1978
- ^ a b Thornborough and Davies 1994, p. 260.
- ^ Lake 1992, p. 199.
- ^ Lake 1992, p. 200.
- ^ Dorr and Bishop 1996, p. 44.
- ^ "Navy MiG Killers" Archived 27 July 2011 at the Wayback Machine, phantomphlyers.org
- ^ a b Grossnick 1997.
- ^ Hunter, Jamie and Collens, Richard. "In Relentless Pursuit of Excellence:VX-30 Bloodhounds" (PDF). Naval Aviation News, September–October 2004, pp. 26–29. Retrieved: 10 November 2015.
- ^ "Marine Fighter Attack Squadron 323".
- ^ Eden 2004, p. 276.
- ^ Lambert, Laura. "Operation Eagle Claw". britannica. Archived from the original on 18 July 2018. Retrieved 17 November 2020.
- ^ Thigpen, Jerry L.; Hobson, James L. (2011). The Praetorian STARShip: The Untold Story of the Combat Talon. Air University Press. p. 210. ISBN 978-1780391977. Archived from the original on 24 January 2023. Retrieved 19 October 2020.
- ^ Eden 2004, p. 277.
- ^ Crowther, M.J.; Baker, Rusty. "The History of VMFA-112" (PDF). Marine Fighter Attack Squadron 112, U.S. Marine Corps. Archived from the original (PDF) on 27 February 2008. Retrieved 13 February 2008.
- ^ "Fact sheet discussing the F-110." Archived 20 December 2014 at the Wayback Machine National Museum of the U.S. Air Force. Retrieved: 26 May 2008.
- ^ a b "McDonnell F-110 Spectre/F-4C Phantom II". Joe Baugher. 12 November 2018. Retrieved 30 September 2024.
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- ^ "History of the 45th Fighter Squadron". 442d Fighter Wing. January 2011. Retrieved 30 September 2024.
- ^ a b Wetterhahn, Ralph (January 2009). "Where Have All the Phantoms Gone?". Air & Space. Archived from the original on 17 June 2013. Retrieved 9 September 2013.
- ^ Dorr and Bishop 1996, p. 38.
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- ^ Dorr and Bishop 1996, p. 232.
- ^ Knaack 1974, p. 274.
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- ^ Handley, Phil. FU Hero Archived 17 February 2015 at the Wayback Machine. fighterpilotuniversity.com. Retrieved
- ^ "The 1989 coup attempt: Unsung heroism, unmasked ploys". December 2021.
- ^ Gordon, Michael R. (2 December 1989). "U.S. Says Bush Used Fighter Jets to Save Aquino from Rebel Siege". The New York Times.
- ^ "Phabulous 40th: Last to Serve." Archived 13 December 2009 at the Wayback Machine Boeing. Retrieved: 19 November 2007.
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- Fricker, John. "Boeing /McDonnell Douglas F-4 Phantom II Current Operators". World Air Power Journal. London: Aerospace, Volume 40, Spring 2000. ISBN 1-86184-043-8.
- Green, William and Gordon Swanborough. The Great Book of Fighters. St. Paul, Minnesota: MBI Publishing, 2001. ISBN 0-7603-1194-3.
- Gimmi, Russell M. Airman: The Life of Richard F. B. Gimmi. Bloomington, Indiana: iUniverse, 2009. ISBN 978-1-4401-5311-2.
- Goodrum, Alastair (January–February 2004). "Down Range: Losses over the Wash in the 1960s and 1970s". Air Enthusiast (109): 12–17. ISSN 0143-5450.
- Grossnick, Roy and William J. Armstrong. United States Naval Aviation, 1910–1995. Annapolis, Maryland: Naval Historical Center, 1997. ISBN 0-16-049124-X.
- Gunston, Bill ed. The Illustrated History of Fighters. New York, New York: Exeter Books Div. of Simon Schuster, 1981. ISBN 0-89673-103-0.
- Gunston, Bill Consulting ed. The Encyclopedia of World Airpower. Crown Publishers, 1979. ISBN 0-517-53754-0.
- Higham, Robin and Carol Williams. Flying Combat Aircraft of USAAF-USAF (Vol.2). Manhattan, Kansas: Sunflower University Press, 1978. ISBN 0-8138-0375-6.
- Hobson, Chris. Vietnam Air Losses, USAF, USN, USMC, Fixed-Wing Aircraft Losses in Southeast Asia 1961–1973. North Branch, Minnesota: Specialty Press, 2001. ISBN 1-85780-115-6.
- Howarth, Alan. Spanish Phantoms and Their Legacy. Air Enthusiast 115, January–February 2005, p. 74ISSN 0143-5450
- Jefford, C.G. RAF Squadrons: A Comprehensive Record of the Movement and Equipment of All RAF Squadrons and Their Antecedents Since 1912:. Shrewsbury, UK: Airlife Publishing, 2nd edition, 2001. ISBN 1-84037-141-2
- Jones, Lloyd S. U.S. Fighters: 1925–1980s. Fallbrook, California: Aero Publishers, Inc., 1975. ISBN 0-8168-9200-8.
- Knaack, Marcelle Size. Encyclopedia of U.S. Air Force Aircraft and Missile Systems: Volume 1 Post-World War II Fighters 1945–1973. Washington, DC: Office of Air Force History, 1978. ISBN 0-912799-59-5.
- Lake Jon. McDonnell F-4 Phantom: Spirit in the Skies. London: Aerospace Publishing, 1992. ISBN 1-880588-04-8.
- List, Friedrich. "German Air Arms Review". Air International, Volume 70, No. 5, May 2006, pp. 50–57. Stamford, Lincolnshire, UK: Key Publishing.ISSN 0306-5634.
- Melampy, Jake. "Phantoms West". Air International, Volume 80, No. 1, January 2011, pp. 36–38. Stamford, Lincolnshire, UK: Key Publishing.ISSN 0306-5634.
- Nordeen, Lon. Fighters Over Israel: The Story of the Israeli Air Force from the War of Independence to the Bekaa Valley. London: Guild Publishing, 1991. ISBN 1-85367-098-7.
- Richardson, Doug and Mike Spick. F-4 Phantom II (Modern Fighting Aircraft, Volume 4) . New York: Arco Publishing, 1984. ISBN 0-668-06068-9.
- Swanborough, Gordon and Peter Bowers. United States Military Aircraft Since 1909. Washington, District of Columbia: Smithsonian, 1989. ISBN 0-87474-880-1.
- Swanborough, Gordon and Peter Bowers. United States Navy Aircraft since 1911. London: Putnam, 1976. ISBN 0-370-10054-9.
- Taylor, Michael J.H. Jane's American Fighting Aircraft of the 20th century. New York: Mallard Press, 1991. ISBN 0-7924-5627-0.
- Thetford, Owen. British Naval Aircraft since 1912. London: Putnam, Fourth Edition, 1994, pp. 254–255. ISBN 0-85177-861-5.
- Thornborough, Anthony M. and Peter E. Davies. The Phantom Story. London: Arms and Armour Press, 1994. ISBN 1-85409-121-2.
- Wagner, Ray. American Combat Planes, Third Enlarged Edition. New York: Doubleday, 1982. ISBN 0-385-13120-8.
- Wilson, Stewart. Phantom, Hornet and Skyhawk in Australian Service. Weston Creek, ACT, Australia: Aerospace Publications, 1993. ISBN 1-875671-03-X.
External links
[edit]- F-4 Phantom II history page on Boeing.com
- F-4 Phantom II Society site
- PhantomF4K.org – Fleet Air Arm – Royal Navy site
- F-4.nl site
- Countering Israeli Reaction to F-4 Sales to Saudi Arabia and Kuwait Archived 20 March 2012 at the Wayback Machine
- 8th Tactical Fighter Wing site
- F-4 Phantom II articles and publications, theaviationindex.com
- The Phantom page with images on fas.org
- ""'Silver Lobos' fly into retirement", af.mil". Air Force. 22 December 2004. Archived from the original on 12 February 2020. Retrieved 23 December 2004.
{{cite web}}: CS1 maint: bot: original URL status unknown (link) - "The Phantom Turns 50" article at Fence Check site
- F-4 Phantom page on Aerospaceweb.org
- RAF Phantom Losses
- The Phantom Zone
- A film clip of McDonnell Douglas F-4 Phantom II is available for viewing at the Internet Archive
- Phantom 50th Anniversary Slideshow
McDonnell Douglas F-4 Phantom II
View on GrokipediaDevelopment
Origins and Design Requirements
In the early 1950s, the United States Navy sought to enhance carrier task force defense against anticipated high-altitude Soviet bombers, prompting the Bureau of Aeronautics to issue requirements for an advanced all-weather fleet interceptor. By 1954, these specifications emphasized a combat radius of approximately 250 nautical miles, endurance for over two hours on patrol, and armament centered on radar-guided Sparrow missiles, with operations from aircraft carriers necessitating robust low-speed handling and arrested landings. The design demanded supersonic performance exceeding Mach 2, a service ceiling approaching 65,000 feet, and twin-engine redundancy for reliability over water.[8] McDonnell Aircraft, having lost the 1953 naval day fighter competition to Vought's F8U Crusader, initiated an unsolicited redesign of its F3H Demon interceptor to meet these needs, evolving the single-seat F3H-G concept into a two-seat configuration for divided pilot and weapons systems officer duties. A mockup of the F3H-G was presented in 1954, incorporating swept wings and initial plans for Wright J65 engines, but McDonnell shifted to General Electric J79 turbojets to achieve the required Mach 2 speeds. On October 18, 1954, the Navy issued a letter of intent for two XF4H-1 prototypes, formalized by a contract on June 25, 1955, prioritizing missile armament over guns to align with emerging air-to-air tactics.[8][9][4] This two-crew, missile-focused approach reflected causal priorities of workload distribution in all-weather intercepts and the perceived obsolescence of guns against fast, distant threats, though later combat experience would challenge the no-gun philosophy. The XF4H-1's airframe featured a low-wing monoplane with 12-degree leading-edge sweep and dogtooth extensions for stability, anhedral tail surfaces, and a semi-monocoque structure optimized for carrier stresses, setting the foundation for multirole adaptability beyond initial interceptor roles.[8][9]Prototype Development and Testing
The McDonnell Aircraft Corporation initiated prototype development for what became the F-4 Phantom II in response to a U.S. Navy requirement for a high-performance, carrier-based interceptor, leading to a contract awarded on July 25, 1955, for two XF4H-1 prototypes and five YF4H-1 pre-production aircraft powered by two General Electric J79-GE-8 turbojet engines each rated at 10,000 lbf dry thrust and 17,000 lbf with afterburner.[10][11] The design emphasized supersonic speed capability up to Mach 2, missile armament including four semi-recessed AIM-7 Sparrow missiles, and advanced radar integration, with the prototypes featuring a two-crew configuration for pilot and radar operator to optimize interception missions.[11] The first prototype, YF4H-1 Bureau Number 142259, conducted its maiden flight on May 27, 1958, at Lambert Field in St. Louis, Missouri, piloted by McDonnell chief test pilot Robert C. Little; the 31-minute flight encountered a hydraulic malfunction that prevented landing gear retraction, and post-flight inspection revealed foreign object damage to the starboard engine.[10][12] Subsequent early test flights quickly demonstrated exceptional performance, surpassing initial expectations by achieving Mach 1.01 shortly after rollout and later reaching speeds up to Mach 2.6 during envelope expansion, validating the airframe's structural integrity and aerodynamic efficiency under high dynamic pressures.[11][13] Following initial company testing, the Navy initiated formal evaluation in late 1958, including a competitive fly-off against the Vought XF8U-3 Crusader III to assess interceptor and fleet defense roles; although the XF8U-3 demonstrated advantages in top speed (Mach 2.39) and maneuverability, the XF4H-1 was selected due to its two-seat configuration that reduced pilot workload with a dedicated radar operator, superior weapon-carrying capacity, and broader mission versatility including air-to-ground tasks, with twin-engine redundancy and payload capacity proving advantageous for long-range operations.[14][15][16] Testing milestones encompassed structural load assessments, weapons delivery trials with early AIM-7 integrations, and high-altitude intercepts, though challenges such as engine reliability issues from ingestion damage required iterative modifications to intake designs and maintenance protocols.[11] By 1959, the prototypes had accumulated sufficient data to support full-scale development, confirming the aircraft's viability despite the loss of the second prototype in a 1960 crash during high-speed testing due to control flutter.[17]Production and Manufacturing Scale
Production of the McDonnell Douglas F-4 Phantom II began in 1958 at the company's facility in St. Louis, Missouri, following the U.S. Navy's initial order for the aircraft as a carrier-based interceptor.[18] McDonnell Aircraft, later McDonnell Douglas after the 1967 merger, manufactured 5,057 units in the United States through 1979, comprising the vast majority of the global total.[19] These included variants for the U.S. Navy, Marine Corps, and Air Force, with allocations of 1,264 for naval service and 2,874 for the Air Force.[19] Manufacturing scale expanded significantly during the Vietnam War era, peaking at 72 aircraft per month in 1967 to meet escalating demand for combat operations.[20] This output rate reflected efficient assembly line processes at the St. Louis plant, where fuselages, wings, and avionics were integrated progressively, enabling the F-4 to become the most-produced American supersonic military aircraft with 5,195 total units worldwide.[21] The final U.S.-built Phantom was delivered on October 24, 1979.[22] License production supplemented U.S. output, primarily in Japan where Mitsubishi Heavy Industries built 138 F-4EJ variants under agreement for the Japan Air Self-Defense Force, concluding with the last rollout in May 1981.[19] No comparable full-scale license manufacturing occurred elsewhere, though exports totaled 919 aircraft to international operators including Israel, Germany, the United Kingdom, and others.[19] The extended run underscored the F-4's versatility across roles, sustaining production for over two decades despite evolving threats.[18]Early Records and Demonstrations
The McDonnell XF4H-1 prototype demonstrated exceptional performance during Operation Top Flight on December 6, 1959, when Commander Lawrence E. Flint, USN, piloted the second aircraft (BuNo. 142260) to a Fédération Aéronautique Internationale absolute altitude record of 98,557 feet (30,040 meters).[23][24] Flint achieved this by accelerating to Mach 2.5 in level flight at 47,000 feet (14,326 meters), initiating a 45-degree climb to 90 degrees, and executing a zoom maneuver that carried the aircraft to the peak altitude before engine shutdown and a dive for relight.[23] This record underscored the Phantom II's high-thrust J79 engines and aerodynamic design, surpassing previous marks set by aircraft like the Lockheed F-104A Starfighter.[24] In September 1960, the F4H-1 further validated its speed capabilities with a world closed-circuit record over a 500-kilometer course, averaging 1,216.78 miles per hour (1,958.16 km/h), set by U.S. Marine Corps Lieutenant Colonel Thomas H. Miller in YF4H-1 BuNo. 142660.[25][5] This achievement, part of a series of Fédération Aéronautique Internationale attempts, highlighted the aircraft's sustained supersonic performance without external stores, contributing to its selection over competitors like the Vought F8U-3 for U.S. Navy service.[25] Project LANA in May 1961 served as a high-profile demonstration of the F4H-1F's long-range potential, involving five aircraft launched from USS Independence (CVA-62) for a non-stop transatlantic crossing to Floyd Bennett Field, New York, with aerial refueling from Douglas A3D-2 Skywarriors.[24][26] Marking the 50th anniversary of U.S. naval aviation (L for 50 in Roman numerals, ANA for Anniversary of Naval Aviation), the flight included a Bendix Trophy competition element, with the lead Phantom averaging over 869 mph cross-country from Los Angeles to New York in a related leg, proving carrier-based interoperability and endurance for fleet defense roles.[24][5] These efforts, conducted under U.S. Navy auspices, amassed 16 world records between 1959 and 1962, with several enduring until the McDonnell Douglas F-15 Eagle's advent, thereby affirming the Phantom II's versatility in speed, altitude, and operational demonstration prior to full-scale production.[25]Design and Engineering
Airframe Structure and Aerodynamics
The F-4 Phantom II features an all-metal semi-monocoque airframe constructed primarily from aluminum alloys, providing structural integrity for high-speed operations and heavy payloads.[4] The fuselage employs a cantilever low-wing monoplane configuration with a length of approximately 58 feet 3 inches and a wingspan of 38 feet 5 inches, optimized for tandem two-seat accommodation and twin-engine mounting.[4] [27] The fuselage incorporates area ruling, a design principle that pinches the cross-section aft of the engine intakes—often described as a "Coke bottle" shape—to minimize transonic wave drag by maintaining a smooth distribution of the airframe's cross-sectional area relative to the Mach cone.[13] This feature enabled sustained supersonic speeds up to Mach 2.2, as the uniform area progression reduces shockwave-induced drag penalties during acceleration through the transonic regime.[27] The semi-monocoque construction distributes loads via stressed skin panels riveted to longerons and bulkheads, supporting internal fuel tanks and weapon bays while accommodating the dorsal engine positioning for improved airflow and reduced radar cross-section elements.[4] The wings utilize a thin, high-speed airfoil section with a 45-degree leading-edge sweep, low aspect ratio (approximately 3.3), and trapezoidal planform to prioritize transonic and supersonic performance over low-speed lift, resulting in high wing loading around 85 pounds per square foot at combat weights.[28] Inner wing sections maintain zero incidence for streamlined high-speed cruise, while outer panels incorporate a 3-degree dihedral (achieved by upward bending of the tips during development) to enhance lateral stability without compromising root structural loads.[28] Automatic leading-edge slats deploy at high angles of attack to improve stall characteristics and low-speed control, complemented by boundary-layer control via engine bleed air blown over trailing-edge flaps to delay flow separation and boost lift coefficients during carrier landings and weapons delivery.[28] The empennage consists of twin vertical stabilizers canted outward at 23 degrees from the vertical to reduce sideslip-induced drag and enhance directional stability at supersonic speeds, paired with a horizontal stabilizer exhibiting anhedral (downward angle) to position it outside the wing's propwash and vortex flow at high angles of attack, thereby preserving pitch control authority.[28] These features contribute to the aircraft's neutral static stability in pitch, relying on fly-by-wire-like pilot inputs and thrust vectoring effects from the widely spaced engines (mounted with slight downward cant) for maneuverability, though the design's high drag at subsonic speeds limited instantaneous turn rates compared to lighter contemporaries.[28] Overall, the Phantom II's aerodynamics emphasize raw speed and payload capacity over agility, embodying a thrust-over-brilliance philosophy where powerful J79 engines compensate for inherent drag limitations in dogfight scenarios.[29]Powerplant and Flight Performance
The McDonnell Douglas F-4 Phantom II was powered by two General Electric J79-GE-series afterburning turbojet engines mounted side-by-side in the rear fuselage. Early U.S. Navy variants, such as the F-4B, employed the J79-GE-8 or J79-GE-10 engines, each delivering 10,900 pounds-force (48.5 kN) of dry thrust and 15,500–17,000 pounds-force (69–76 kN) with afterburner.[30][4] Later models, including the F-4E, incorporated upgraded J79-GE-17 engines providing 11,870 pounds-force (52.8 kN) dry and 17,900 pounds-force (79.6 kN) with afterburner per engine, enhancing overall thrust by approximately 900 pounds-force each over prior versions.[31][32] These engines featured axial compressors, annular combustors, and variable-area exhaust nozzles for afterburner operation, enabling supersonic performance but producing characteristic black smoke trails due to fuel-rich combustion, a trait mitigated in some export variants with smoke-reducing modifications.[33] Flight performance emphasized high speed and altitude capability suited for interception and strike roles. The Phantom II attained a maximum speed of Mach 2.23 (approximately 1,473 mph or 2,370 km/h) at 40,000 feet (12,200 meters), with cruise speeds around 585 mph (940 km/h).[34][35] Service ceiling reached 59,600 feet (18,200 meters), allowing operations above most contemporary threats.[2][36] Combat radius varied by loadout but typically measured 367 nautical miles (422 miles or 680 km) with external stores, while ferry range extended to 1,615 miles (2,600 km) with drop tanks.[34][37]| Performance Parameter | Value |
|---|---|
| Maximum Speed | Mach 2.23 at 40,000 ft |
| Cruise Speed | 585 mph (940 km/h) |
| Service Ceiling | 59,600 ft (18,200 m) |
| Combat Radius | 367 nmi (680 km) |
| Ferry Range | 1,615 mi (2,600 km) |
Armament and Weapon Systems Evolution
The McDonnell Douglas F-4 Phantom II entered U.S. Navy service in 1961 as a missile-armed interceptor without an internal cannon, emphasizing speed, range, and payload over close-range firepower. Its primary armament consisted of up to four AIM-7 Sparrow semi-active radar-homing missiles for beyond-visual-range engagements and four AIM-9 Sidewinder infrared-homing missiles for shorter ranges, supported by the AN/APQ-72 radar. The aircraft featured nine external hardpoints capable of carrying up to 16,000 pounds of ordnance, including secondary loads of unguided bombs or rockets, though early operations prioritized fleet defense over ground attack.[3][39][40] Combat experience in the Vietnam War, beginning in 1965, exposed limitations in the missile-only doctrine, as subsonic dogfights often occurred within visual range where missile reliability suffered from launch parameters, electronic countermeasures, and visual acquisition challenges. U.S. forces initially adapted by mounting external gun pods, such as the SUU-16/A (introduced around 1966), which carried a 20 mm M61 Vulcan cannon with 1,200 rounds, later upgraded to the SUU-23/A for improved performance; these were fitted to the centerline station and integrated with a lead-computing optical gunsight like the ASG-22. The U.S. Air Force's F-4C and F-4D variants incorporated wiring and pylons for these pods, enabling temporary gun capability without major airframe redesign.[39][40] This interim solution evolved into a permanent fixture with the F-4E variant, which entered production in 1967 and featured an internal M61A1 Vulcan 20 mm rotary cannon housed in a redesigned nose section, provisioned with 640 rounds of ammunition. The addition addressed dogfighting deficiencies empirically demonstrated in Vietnam, where gun kills proved decisive in several engagements, enhancing the Phantom's versatility as a multirole fighter capable of air superiority and close air support. Concurrently, ground-attack armament expanded to include precision-guided munitions like the AGM-65 Maverick missile and cluster bomb dispensers on underwing pylons, while air-to-air missiles progressed to improved variants such as the AIM-7E/F and AIM-9D/G. Navy Phantoms, including upgraded F-4N and F-4S models, retained the no-cannon configuration but continued using pods and advanced missiles like the AIM-7M into the 1980s.[41][39][40] Specialized variants further diversified the weapon systems: the F-4G "Wild Weasel," converted from F-4Es starting in the late 1970s, integrated anti-radiation missiles such as the AGM-45 Shrike (later supplemented by the AGM-88 HARM in the 1980s) for suppression of enemy air defenses, underscoring the Phantom's adaptation from interceptor to dedicated electronic warfare platform. These evolutions reflected causal lessons from operational data, prioritizing empirical combat effectiveness over initial design assumptions of missile dominance in air warfare.[40]Avionics, Radar, and Electronics
The McDonnell Douglas F-4 Phantom II's avionics emphasized multi-role capabilities through integrated radar, navigation, and electronic warfare systems, operated primarily by a two-person crew consisting of a pilot and a radar intercept officer (RIO) or weapons systems officer (WSO). Early variants relied on analog instrumentation and pulse radars optimized for beyond-visual-range engagements with semi-active radar-homing missiles like the AIM-7 Sparrow.[33] The cockpit featured tandem seating with the RIO positioned aft, monitoring a dedicated radar display and managing missile guidance, while the pilot handled flight controls via conventional stick and rudder inputs augmented by hydraulic systems.[42] Primary radar systems evolved to address limitations in ground clutter rejection and multi-target tracking. The initial F4H-1 and F-4B models incorporated the AN/APQ-72, an X-band pulse radar with a 32-inch (81 cm) parabolic reflector antenna, enabling detection and tracking for Sparrow missile intercepts but lacking pulse-Doppler processing for low-altitude targets.[43] Subsequent U.S. Air Force variants upgraded to more capable units: the F-4D received the AN/APQ-109, which supported guidance for television-guided munitions like the AGM-62 Walleye, while the F-4E introduced the Westinghouse AN/APQ-120 in 1967, a fully solid-state X-band pulse-Doppler fire-control radar with an instrumented range of about 93 km, improved look-down/shoot-down capability, and integration for the aircraft's internal M61 Vulcan cannon.[44][45][46] Electronic countermeasures and warning systems were integral, with early Phantoms equipped with the AN/APR-25 and AN/APR-26 radar warning receivers for threat detection.[47] The AN/APR-38 Radar Homing and Warning (RHAWS) system, tested on F-4D prototypes in 1972, provided enhanced directional threat localization and formed the basis for the F-4G Wild Weasel's advanced suppression of enemy air defenses suite, incorporating the AN/APR-38/47 for real-time emitter identification and targeting of anti-radiation missiles like the AGM-45 Shrike.[47][48] Navigation and communication electronics included TACAN for tactical air navigation, UHF radios for voice coordination, and the AN/APX-80 Combat Tree interrogator pod, first deployed on F-4s during the Vietnam War, which enabled identification of hostile MiG fighters via datalink compatibility with U.S. airborne early warning platforms, significantly improving situational awareness in contested airspace.[49] Later upgrades in variants like the F-4S incorporated slatted wings alongside avionics enhancements such as improved hydraulics and wiring for reliability, though core systems remained analog until retirement.[4]| Variant | Primary Radar | Key Features |
|---|---|---|
| F-4B | AN/APQ-72 | X-band pulse radar; 81 cm antenna; BVR missile support[43] |
| F-4D | AN/APQ-109 | Compatible with AGM-62 Walleye; upgraded avionics suite[44] |
| F-4E | AN/APQ-120 | Solid-state pulse-Doppler; ~93 km range; cannon integration[45][46] |
Operational Costs and Logistics
The McDonnell Douglas F-4 Phantom II imposed substantial operational costs on its operators, driven by high fuel demands, intensive maintenance, and logistical complexities associated with its large airframe and advanced systems. During its primary service period, the aircraft's cost per flight hour was approximately €10,000 (equivalent to about $11,000 USD), a figure elevated by the need for frequent servicing of its twin General Electric J79 engines and radar systems, which were prone to wear under high-utilization combat conditions.[50] Later variants and aging fleets saw costs rise further; for instance, South Korean F-4 operations in the 2020s reached $23,000 per flight hour, encompassing fuel, parts, and manpower amid diminishing spares availability.[51] Fuel consumption represented a major expense, with the F-4 carrying up to 16,000 pounds for typical missions but expending it rapidly during operations. At a cruise speed of 450 knots, the aircraft consumed roughly 100 pounds of JP-4 or JP-5 fuel per minute, escalating dramatically in afterburner to 120,000 pounds per hour, which limited endurance without aerial refueling and strained forward-area supply lines.[52][53] This thirst for fuel, combined with the need for external drop tanks in extended missions, necessitated extensive tanker support, particularly in theater deployments like Vietnam where sortie generation rates amplified logistical burdens. Logistically, the F-4 required a two-person crew—a pilot and weapons systems officer—adding to training and personnel overhead, while ground maintenance demanded specialized technicians for its 18,000-pound weapons loadout and nine hardpoints, often exceeding 20 man-hours per flight hour in sustained operations. Parts distribution networks were critical, with centralized depots supplying engines, avionics, and tires to dispersed bases, but challenges arose in remote or contested areas, such as Vietnam's humid environment accelerating corrosion and component failures. High attrition rates—over 500 U.S. F-4s lost in Southeast Asia—further stressed inventories, prompting rapid production surges and international co-production to sustain fleets. These factors contributed to the aircraft's eventual phase-out in favor of more efficient designs, as escalating sustainment costs outweighed its versatility by the 1980s and 1990s.[50]U.S. Operational History
Navy and Marine Corps Service
The McDonnell F-4 Phantom II originated as a carrier-based interceptor for the United States Navy, with prototype flights commencing on May 27, 1958, and initial deliveries to Navy and Marine Corps squadrons starting in 1960.[28][3] The aircraft achieved operational status with Navy fighter squadrons in 1961, equipping units such as VF-74 for carrier deployments aboard vessels like USS Independence.[3] Its versatility enabled rapid adaptation for multi-role missions, including air superiority, ground attack, and reconnaissance, supported by tandem two-seat configuration for pilot and radar intercept officer.[54] The Navy's primary production variant, the F-4B, totaled 649 units built for joint Navy and Marine Corps procurement, featuring General Electric J79 turbojet engines and capability for AIM-7 Sparrow and AIM-9 Sidewinder missiles.[55] The United States Marine Corps received its first F-4Bs in June 1962, assigning them to VMFA-314 at Marine Corps Air Station El Toro, California, for close air support and fighter roles integrated with amphibious operations.[3] Marine squadrons, designated VMFA, operated the Phantom from land bases and carriers, emphasizing tactical flexibility in expeditionary environments, with units like VMFA-314 deploying for early combat evaluations.[54] Subsequent upgrades addressed aerodynamic and avionics limitations; the F-4J variant, entering Navy and Marine service around 1967, incorporated improved radar and multi-channel communications, with 522 produced.[55] In the 1970s, the Service Life Extension Program refurbished older airframes: 228 F-4Bs became F-4Ns with strengthened structures and avionics enhancements, while select F-4Js were modified to F-4S standard, adding leading-edge slats for better low-speed handling on carriers.[3] These variants sustained frontline utility through the 1980s, with the F-4 conducting its final Navy fleet deployments in electronic warfare and strike roles. Navy retirement progressed with F-4Ns phased out from active deployable squadrons by 1984, followed by F-4Ss in 1987, as F-14 Tomcats and F/A-18 Hornets assumed primary fighter duties.[54] Marine Corps operations persisted longer, with VMFA-112 retiring the last active F-4S on January 18, 1992, transitioning to F/A-18s amid post-Cold War force reductions.[56] Throughout its service, the Phantom amassed over 5,195 total production units across variants, underscoring its role in carrier air wings and Marine aviation for nearly three decades.[3]Air Force Adoption and Roles
The United States Air Force initially evaluated the F-4 Phantom II for potential adoption following its success in U.S. Navy service, conducting trials in interceptor, attack, and close air support roles during the early 1960s.[57] Despite preferences for lighter, single-engine fighters aligned with Air Force doctrine emphasizing maneuverability, the Phantom's demonstrated speed, payload capacity, and versatility prompted a shift. Production of the USAF-specific F-4C variant was authorized on February 8, 1963, marking formal adoption after evaluations confirmed its multi-role capabilities superior to alternatives in certain metrics.[4] The F-4C entered operational service with the USAF's 12th Tactical Fighter Wing at MacDill Air Force Base, Florida, in early 1964, initially tasked with air defense and tactical fighter missions.[2] Subsequent variants like the F-4D and F-4E incorporated improvements such as enhanced avionics and internal gun provisions, expanding its utility. By the mid-1960s, the Phantom had become the USAF's primary tactical fighter, equipping numerous wings for continental air defense and overseas deployments.[58] In service, the F-4 fulfilled diverse roles including air superiority, interdiction, close air support, and reconnaissance via the RF-4C variant.[38] It conducted air-to-air intercepts, ground attack strikes, and suppression of enemy air defenses (SEAD) as the "Wild Weasel" configuration, with over 116 F-4Es modified for radar detection and anti-radiation missile employment.[28] The aircraft's adaptability allowed integration into strategic bombing support and tactical nuclear delivery, underscoring its evolution from a Navy interceptor to a cornerstone of USAF multi-role operations through the 1970s and beyond.[59]Vietnam War Engagements
The McDonnell Douglas F-4 Phantom II first engaged in combat operations over Vietnam on August 5, 1964, when U.S. Navy F-4Bs from USS Constellation provided escort for A-4 Skyhawks during Operation Pierce Arrow strikes against North Vietnamese naval vessels.[60] The aircraft's initial air-to-air victory occurred on June 17, 1965, when an F-4B from VF-21, piloted by Commander Louis Page with Lieutenant John C. Smith as radar intercept officer, downed a MiG-17 using an AIM-9 Sidewinder missile.[61] During Operation Rolling Thunder, from March 2, 1965, to November 2, 1968, F-4s served as primary interceptors and escorts for bombing missions against North Vietnam, facing Soviet-supplied MiG-17s, MiG-19s, and MiG-21s. Early engagements revealed limitations in the F-4's missile reliability and lack of an internal gun, contributing to unfavorable exchange ratios; for instance, U.S. forces lost five F-4s to MiG-21s in 1965-1966 while achieving few confirmed kills.[6] Tactics evolved with improved AIM-7 Sparrow guidance and pilot training, exemplified by Operation Bolo on January 2, 1967, where 8th Tactical Fighter Wing F-4s, mimicking F-105 Thunderchief formations, ambushed and destroyed seven MiG-21s without loss.[62] U.S. F-4 variants achieved approximately 150 MiG kills across services, with U.S. Air Force Phantoms credited with 108, Navy with 40, and Marines with 3, primarily using AIM-7 and AIM-9 missiles.[6] In ground attack roles, F-4s delivered ordnance in missions like close air support and interdiction, with F-4Ds introducing precision-guided munitions later in the war.[63] F-4C and F-4G models adapted for Wild Weasel suppression of enemy air defenses (SEAD) from 1966 onward, employing AGM-45 Shrike anti-radiation missiles to target SA-2 SAM sites, though at high risk with dedicated crews suffering significant losses.[64] Overall, 445 U.S. Air Force F-4s were lost in Southeast Asia, including 370 in combat—33 to MiGs, 30 to SAMs, and 307 to antiaircraft artillery—with total U.S. military F-4 combat losses exceeding 500.[56] Despite these attrition rates, driven largely by ground fire rather than air-to-air combat, the F-4's versatility enabled it to maintain air superiority and support bombing campaigns, with later adaptations yielding kill ratios exceeding 5:1 in 1972 operations like Linebacker.[65]Post-Vietnam U.S. Operations
Following the end of U.S. involvement in Vietnam in 1975, the U.S. Navy and Marine Corps continued operating F-4 Phantoms in carrier-based fighter and attack roles, conducting routine deployments to the Atlantic, Pacific, and Mediterranean regions for air defense and strike training until the mid-1980s.[54] The last deployable Navy F-4S squadrons retired in 1987, with the aircraft fully phased out of fleet service by 1988 after 26 years of active duty, replaced primarily by the F-14 Tomcat and F/A-18 Hornet.[54] The U.S. Air Force retained F-4 variants longer for tactical fighter, reconnaissance with RF-4Cs, and suppression of enemy air defenses (SEAD) missions, with the specialized F-4G Advanced Wild Weasel entering service after modifications from F-4E airframes beginning in 1975.[66] The F-4G featured the AN/APR-47 electronic warfare system in place of the internal cannon, enabling detection and targeting of enemy radars, armed with AGM-88 HARM anti-radiation missiles for standoff attacks up to 52 miles, alongside AGM-45 Shrike, AGM-65 Maverick, AIM-7 Sparrow, and AIM-9 Sidewinder for self-defense.[66][67] In Operation Desert Shield, F-4Gs from the 35th Tactical Fighter Wing at George AFB, California, and the 52nd Tactical Fighter Wing at Spangdahlem Air Base, Germany, deployed to Shaikh Isa Air Base, Bahrain, arriving on August 12, 1990.[68] During Operation Desert Storm starting January 17, 1991, these units, including the 81st and 561st Tactical Fighter Squadrons, flew 3,942 combat sorties over 42 days, launching over 1,000 air-to-ground missiles and destroying 200 Iraqi surface-to-air missile sites while contributing to the neutralization of 74% of enemy missile radars.[68][67] Tactics involved the "Magnum" call to signal HARM launches, prompting Iraqi operators to shut down radars preemptively, thus clearing paths for strikes by F-16Cs, B-52s, and F-111s; the 81st TFS alone achieved 142 confirmed SAM-site kills across 4,000 combat hours.[67] One F-4G was lost on January 18, 1991, to fuel starvation with the crew ejecting safely, but no aircraft were downed by enemy fire in missions supported by Wild Weasels.[68][67] The F-4G's combat role in Desert Storm represented the Phantom II's final major U.S. operational deployment, with the variant retired by the 190th Fighter Squadron of the Idaho Air National Guard in October 1995 and fully phased out of USAF service by 1996.[68][66]International Service
Major Export Users and Adaptations
The McDonnell Douglas F-4 Phantom II was exported to 11 nations outside the United States, with Germany receiving the largest single order of 175 F-4F interceptors optimized for air superiority, lacking the internal cannon of the F-4E but later upgraded via the ICE program to incorporate AN/APG-65 radar and AIM-120 AMRAAM missiles by 1998.[69] Germany also acquired 88 RF-4E reconnaissance variants starting in 1971 for tactical intelligence roles.[69] Israel imported 204 F-4E fighters beginning in September 1969, supplemented by 12 RF-4E reconnaissance aircraft, and conducted extensive modifications including the Phantom 2000 upgrade in 1989 that enhanced avionics and structural life, with a Super Phantom 2000 prototype tested in 1987 featuring canard foreplanes for improved maneuverability.[69] The Israeli Air Force integrated these with indigenous systems like TISEO radar for aerial identification.[69] The United Kingdom operated 52 F-4K (FG.1) variants for the Royal Navy and 118 F-4M (FGR.2) for the Royal Air Force, both adapted with Rolls-Royce Spey turbofan engines for better low-speed performance on carriers and British avionics including Skyflash missiles, with later rewinging of FGR.2s from 1987 to extend service life until retirement in 1992.[69] Japan licensed production of 138 F-4EJ fighters and 14 RF-4E reconnaissance aircraft from 1971 to 1981 under Mitsubishi, featuring Japanese avionics and later upgraded to F-4EJ Kai standard between 1989 and 1995 with AN/APG-66J radar for improved air-to-air capabilities, serving until retirement in 2020.[69] Other significant users included Turkey with 192 F-4E and 40 RF-4E acquired from 1974, upgraded to Phantom 2020 standard in 1999 by Israel Aerospace Industries for extended structural integrity and avionics; Iran with 251 total F-4D/E and RF-4E from 1968, maintained through indigenous upgrades including service-life extensions in 2008 despite sanctions; Greece with 84 F-4E and 37 RF-4E from 1974, modernized in 1997-1999 to carry AIM-120 missiles; and South Korea with 207 F-4D/E and 12 RF-4C from 1969, retired in 2023 after structural reinforcements and Pave Tack pod integrations.[69][70]| Country | Primary Variants | Approximate Number Acquired | Key Adaptations |
|---|---|---|---|
| Germany | F-4F, RF-4E | 175 F-4F, 88 RF-4E | Simplified air superiority design; ICE upgrade with AMRAAM |
| Israel | F-4E, RF-4E | 204 F-4E, 12 RF-4E | Phantom 2000 avionics; structural mods |
| UK | F-4K/FG.1, F-4M/FGR.2 | 52 F-4K, 118 F-4M | Spey engines; British avionics and missiles |
| Japan | F-4EJ, RF-4E | 138 F-4EJ, 14 RF-4E | Licensed build; Kai upgrade with new radar |
| Turkey | F-4E, RF-4E | 192 F-4E, 40 RF-4E | Phantom 2020 upgrade |
| Iran | F-4D/E, RF-4E | 235 F-4D/E, 16 RF-4E | Indigenous avionics and probe mods |
Combat Use by Allies
The Israeli Air Force introduced F-4E Phantom II variants, designated Kurnass, in September 1969 and immediately committed them to the War of Attrition along the Suez Canal, with the first combat mission occurring on October 22, 1969, and the initial aerial victory—a MiG-21—recorded on November 11, 1969.[71] During the Yom Kippur War on October 6, 1973, F-4s equipped seven squadrons and served as the primary fighter, executing deep strikes and air superiority missions that contributed to downing 116.5 enemy aircraft across Israeli Phantom operations.[71] In the 1982 Lebanon campaign, Israeli F-4s spearheaded Operation Mole Cricket 19 on June 9, systematically destroying 19 Syrian SAM batteries in the Bekaa Valley, demonstrating effective suppression of enemy air defenses through coordinated tactics and modifications enhancing radar and armament integration.[71] [72] The Iranian Air Force operated F-4D and F-4E Phantoms, acquired prior to the 1979 revolution, extensively during the Iran-Iraq War from 1980 to 1988, focusing on strategic bombing of infrastructure like the Osirak nuclear reactor struck in September 1980 and oil facilities such as the Az-Zubayr field.[73] In November 1980's Operation Morvarid, F-4s supported naval strikes that neutralized much of Iraq's surface fleet during the Tanker War phase, employing Maverick missiles against shipping.[73] Despite U.S. sanctions limiting spares, Iranian crews conducted low-altitude interdictions and cluster bomb runs, though the fleet of approximately 230 aircraft incurred losses nearing 50% from ground fire and intercepts.[73] Turkey's Air Force received F-4E Phantoms in 1974 and deployed them amid the Cyprus crisis that year, participating in air support and the largest combat aviation effort in Turkish history up to that point, including strikes against Greek Cypriot positions.[74] Subsequent upgrades enabled precision ground attacks against PKK insurgent targets into the 1990s and beyond, with the aircraft retaining air-to-ground roles despite phasing out air-to-air missions by the mid-1980s due to radar limitations against evolving threats.[75]Current Operational Status
As of July 2025, approximately 98 McDonnell Douglas F-4 Phantom II aircraft remain in active military service worldwide, primarily in multirole fighter-bomber and reconnaissance capacities despite their advanced age exceeding 50 years for most airframes.[76] These survivors operate under the air forces of Greece, Turkey, and Iran, with no active U.S. or other former major operators retaining combat-ready examples following South Korea's formal retirement of its fleet on June 7, 2024, after 55 years of service.[77][76] The Hellenic Air Force of Greece maintains a fleet of around 33 F-4E variants, configured for air-to-ground strikes and air superiority missions, though operations are gradually scaling back in favor of newer platforms like the Rafale.[78] Upgrades have extended their viability, including improved avionics and precision-guided munitions integration, but structural fatigue and parts scarcity pose ongoing challenges amid plans for full phase-out within the decade.[79] Turkey's Turkish Air Force continues to fly upgraded F-4E 2020 "Terminator 2020" models, with enhancements to radar, electronic warfare systems, and targeting pods enabling low-altitude penetration and standoff weapon employment; these aircraft marked 50 years of service in November 2024 with high-profile flights demonstrating sustained combat readiness.[80][81] The fleet supports NATO commitments, including reconnaissance over the Aegean and Black Sea regions, though eventual replacement by F-16 upgrades and indigenous designs like the TF-X is anticipated.[79] Iran's Islamic Republic of Iran Air Force sustains an estimated 20-30 F-4D/E and RF-4E aircraft, originally acquired pre-1979 Revolution, for tactical strikes and photo-reconnaissance despite U.S. sanctions limiting spares and overhauls; indigenous modifications, such as reverse-engineered engines and domestically produced munitions, have kept select units airworthy for regional deterrence roles.[82][76] Operational tempo remains low due to maintenance constraints, with reliance on stored airframes for attrition replacements.[83] No other nations report active combat fleets, though decommissioned examples from South Korea have been eyed for civilian conversion, such as aerial target towing or experimental space-launch platforms, without restoring fighter capabilities.[79]Combat Effectiveness Evaluation
Tactical Strengths and Achievements
The McDonnell Douglas F-4 Phantom II exhibited superior tactical strengths rooted in its aerodynamic design and powerplant, achieving a maximum speed exceeding Mach 2.2 at altitude and a combat radius suitable for long-range interdiction missions.[1] Its twin General Electric J79 turbojet engines provided thrust-to-weight ratios enabling rapid acceleration and sustained supersonic performance, while the airframe's robustness allowed it to carry up to 18,000 pounds of ordnance across nine external hardpoints, including air-to-air missiles, bombs, and rockets.[84] This payload capacity, combined with a large internal fuel load, facilitated multi-role operations from interception to close air support without compromising speed or maneuverability.[7] Equipped with the AN/APQ-72 radar, the F-4 was the first operational fighter capable of independent target detection and all-weather engagement, enhancing its effectiveness in low-visibility conditions and beyond-visual-range combat.[13] The system's integration with semi-active radar-homing missiles like the AIM-7 Sparrow allowed for intercepts at distances up to 50 miles, a significant advantage over visually reliant adversaries.[85] In terms of achievements, the Phantom II set 16 Fédération Aéronautique Internationale (FAI) world records between 1959 and 1962, including an absolute speed record of 1,606.342 miles per hour established on December 22, 1961, during Operation Skyburner with water-methanol injection modifications.[25] It also claimed an absolute altitude record of 98,556 feet in 1959, demonstrating exceptional climb rates and ceiling capabilities that underscored its engineering prowess.[86] Five of these records endured until surpassed by the McDonnell Douglas F-15 Eagle in the 1970s.[25] During the Vietnam War, F-4 crews achieved notable successes following doctrinal shifts emphasizing close-range tactics and formation discipline, such as Operation Bolo on January 2, 1967, where the U.S. Air Force's 8th Tactical Fighter Wing downed seven North Vietnamese MiG-21s without losses by mimicking F-105 Thunderchief flight profiles.[87] Colonel Robin Olds, commanding the 8th TFW, personally scored four MiG victories in his F-4C Phantom named Scat XXVII across 152 missions.[88] U.S. forces credited the F-4 with downing over 100 enemy fighters, contributing to the only five American aces of the conflict—all flying Phantoms.[89] Israeli Air Force F-4s further validated these strengths in the 1973 Yom Kippur War, where superior pilot training and radar-guided weaponry yielded air-to-air kill ratios exceeding 10:1 in engagements against Arab MiGs and Sukhois, despite numerical disadvantages.[90] Overall, IDF/AF Phantom units amassed 116.5 confirmed aerial victories from 1969 to 1982, highlighting the aircraft's adaptability when paired with skilled operators.[91]Design Limitations and Early Shortcomings
The McDonnell Douglas F-4 Phantom II's initial design omitted an internal cannon, aligning with the U.S. Navy's 1950s doctrine favoring guided missiles for supersonic intercepts beyond visual range. Early armament relied on the AIM-7 Sparrow radar-guided missile and AIM-9B Sidewinder infrared missile, but these suffered from low reliability in operational conditions; the AIM-9B, for instance, achieved a 28% hit rate in Vietnam despite manufacturer claims of 65%. The absence of a gun forced pilots to use unreliable external pods like the GAU-4, which the Navy employed briefly but ineffectively, exacerbating vulnerability in close-range engagements where missiles often failed to acquire locks or detonate properly due to lacking proximity fuses.[85][92] Aerodynamic compromises for high-speed performance and heavy payload capacity resulted in high wing loading, producing a wide turning radius and significant energy bleed in sustained turns. Hard-wing variants without leading-edge slats exacerbated this, with pilots noting the aircraft "hemorrhaged speed while turning" owing to its large size and drag profile, enabling lighter foes like the MiG-17 to position for attacks from inside the F-4's turn. Adverse yaw at high angles of attack further risked spins without stability augmentation, demanding precise handling that strained less experienced crews.[92][85][93] The General Electric J79 engines generated prominent smoke trails visible up to 25 miles distant, undermining surprise in visual combat and reconnaissance missions. Early production aircraft also faced structural and systems shortcomings, including fuel tank leaks necessitating post-flight resealing, cracks in outer wing ribs on approximately 85 F-4s, faulty aileron control cylinders, electrical connector failures, and recurrent engine compartment fires. These issues, combined with the two-seat layout's added weight and restricted rearward visibility, highlighted the trade-offs in the F-4's multirole versatility during its 1961 entry into Navy service and subsequent Air Force adoption.[92][49][85]Adaptations, Improvements, and Kill Ratios
Early F-4 Phantom II variants, such as the F-4B and F-4C, lacked an internal cannon and depended on AIM-7 Sparrow and AIM-9 Sidewinder missiles, which exhibited low success rates—often below 10% for Sparrows—in Vietnam's close-range dogfights exacerbated by rules of engagement limiting beyond-visual-range shots.[94][95] This contributed to initial U.S. kill ratios of approximately 2:1 during Rolling Thunder (1965–1968), with 118 MiG kills against 55 F-4 losses in air-to-air combat.[94] To address dogfighting deficiencies, the U.S. Air Force fitted F-4s with SUU-16/A gun pods starting in April 1967, securing 4 MiG kills from 8 firings.[94] The F-4E variant integrated an M61A1 Vulcan 20mm cannon, with first production aircraft flying on June 30, 1967, and operational deployment to Vietnam in November 1968; by mid-1971, 72 F-4Es equipped with the gun served in theater.[94][13] Later F-4E models incorporated leading-edge slats for enhanced maneuverability at low speeds, while missile upgrades included the AIM-9D Sidewinder with cooled seeker in June 1966 and AIM-9G in 1972, achieving a 46% kill probability (23 kills from 50 launches).[94][28] Tactical and systemic adaptations further elevated performance. The Navy's Top Gun school, established in March 1969, emphasized within-visual-range combat skills, elevating MiGCAP kill ratios to 6.4:1 overall and contributing to a 12:1 ratio for Navy F-4s from January 1972 to January 1973.[95][94] The Air Force's Teaball battle management system, operational from August 1972, integrated ground-controlled radar and intelligence to provide real-time warnings, improving USAF MiGCAP ratios to 5.5:1 overall and peaking at 15:1 in the war's final months.[95] Additional enhancements in later variants like the F-4J (from December 1966) featured reduced-smoke J79-GE-10 engines to minimize detectability.[96] These modifications yielded overall F-4 kill ratios exceeding 3:1 in Vietnam, with U.S. forces crediting Phantoms for over 150 MiG victories against roughly 40 air-to-air losses, though North Vietnamese claims disputed higher U.S. losses; USAF totals reached 137 kills against 64 fixed-wing losses (including non-air-to-air), while Navy Phantoms downed 56 MiGs for 12 air-to-air losses.[95][6] Post-Vietnam upgrades, such as the F-4S's slat modifications and avionics enhancements, sustained adaptability into the 1980s, informing successor designs like the F-15 with inherent guns and superior agility from inception.[96]Retirement, Preservation, and Legacy
Phasing Out and Replacements
The United States Air Force phased out the F-4 Phantom II from frontline active-duty units between 1992 and 1995 as more capable fourth-generation fighters entered widespread service.[13] The F-15 Eagle assumed primary air superiority roles, offering superior speed, maneuverability, and radar capabilities, while the F-16 Fighting Falcon handled multirole fighter-bomber duties with enhanced agility and lower operating costs.[82] Air National Guard squadrons continued limited operations into the mid-1990s, with the last F-4G Wild Weasel electronic warfare variant retired in 1996.[97] Converted QF-4 drones provided target services until their final flight on December 21, 2016, at Holloman Air Force Base, marking the end of all U.S. military F-4 operations.[98][97] The U.S. Navy completed its F-4 retirement by 1987, transitioning carrier-based squadrons to the Grumman F-14 Tomcat for long-range interception and fleet air defense, which featured variable-sweep wings and the advanced AWG-9 radar.[54][99] The U.S. Marine Corps followed suit, adopting the F/A-18 Hornet as a versatile strike fighter with improved short-field performance and multirole avionics suited to amphibious operations.[100] Across the services, the shift reflected the F-4's aging airframe, high maintenance demands from Vietnam-era wear, and the need for fly-by-wire controls and beyond-visual-range missile integration absent in later upgrades.[101] International operators extended F-4 service through local modifications, delaying full phase-outs until the 2000s and 2010s. The German Luftwaffe retired its F-4F fleet in 2013, replacing it with Eurofighter Typhoons for air defense.[102] Japan's Air Self-Defense Force decommissioned F-4EJs in March 2021, succeeded by upgraded F-15J variants.[102] South Korea's Republic of Korea Air Force ended operations in June 2024 after 55 years, transitioning to F-15K and F-35A aircraft for enhanced strike and stealth capabilities.[103] Turkey maintains upgraded F-4E Terminators for ground attack, with no immediate replacement announced as of 2024, leveraging structural reinforcements and precision-guided munitions to sustain viability against regional threats.[80] These prolongations stemmed from cost-effective upgrades offsetting the F-4's obsolescent radar cross-section and engine efficiency compared to peers like the F-16 or Mirage 2000 adopted elsewhere.[81]Surviving Aircraft and Displays
Numerous McDonnell Douglas F-4 Phantom II aircraft survive in preserved condition, primarily as static displays in aviation museums and at former military bases, representing variants from U.S. and international operators. Preservation efforts focused on historically significant airframes, often those with combat records or prototype status, amid widespread scrapping of retired examples for parts or conversion to target drones under the QF-4 program. In the United States, where the majority of preserved Phantoms reside, museums house airframes from Air Force, Navy, and Marine Corps service, showcasing the type's evolution from interceptor to multirole fighter. The National Museum of the United States Air Force displays F-4C serial 64-0674, credited with two MiG-17 kills in a single mission over North Vietnam on May 4, 1967, by pilot Colonel Robin Olds and weapons systems officer Lieutenant Stephen Croker.[2] The Steven F. Udvar-Hazy Center of the National Air and Space Museum exhibits F-4S Bureau Number 153915, a Navy variant upgraded with leading-edge slats and smokeless engines for improved maneuverability.[4] Hill Aerospace Museum preserves F-4D serial 66-7495, highlighting the Air Force's early adoption and modifications for nuclear strike roles.[104] Additional U.S. examples include F-4N 152287 at the National Naval Aviation Museum, representing post-Vietnam service life extensions, and F-4E at Wings Over the Rockies Air & Space Museum, equipped with the M61 Vulcan cannon pod.[105][41] Internationally, preserved Phantoms reflect export adaptations, such as the F-4K prototype at the UK's Fleet Air Arm Museum in Yeovilton, the earliest British variant with Rolls-Royce Spey engines for carrier operations.[106] Private preservation includes the Collings Foundation's F-4D serial 66-7554, acquired from storage at Davis-Monthan AFB and maintained for potential flight training and demonstration, though currently undergoing heavy maintenance as of 2025.[63] Restoration projects, like F4H-1F Bureau Number 145310 under private ownership, aim to return early prototypes to airworthy condition, underscoring ongoing interest in the Phantom's engineering amid limited surviving flyable examples outside active militaries.[107]Modern and Civilian Applications
Following retirement from manned combat roles, surplus McDonnell Douglas F-4 Phantom II airframes were adapted into QF-4 unmanned aerial targets for U.S. military weapons testing and adversary simulation. These remotely piloted vehicles, modified by BAE Systems, replicated enemy fighter maneuvers to evaluate air-to-air missiles and radar systems, with over 300 conversions completed by 2012.[108] The program operated reusable, full-scale drones capable of takeoff, navigation, and landing under ground control, primarily at ranges like White Sands Missile Range. The final QF-4 unmanned flight occurred on August 17, 2016, marking the end of Phantom II service in any U.S. capacity.[109][110][111] In civilian applications, the Collings Foundation maintains the only privately owned F-4D Phantom II in North America, obtained through a special act of Congress to enable public education and airshow performances. This aircraft has demonstrated aerobatic capabilities, including victory rolls and high-speed passes, at events like the Thunder Over Michigan Airshow. As of 2025, it remains grounded for heavy maintenance but holds potential for future flight training programs and heritage flights.[63][112][113] No other civilian operators conduct routine flights, though static displays in museums support aviation history preservation.[114]Enduring Engineering Lessons
The F-4 Phantom II's initial armament philosophy, which omitted an internal cannon in favor of radar-guided AIM-7 Sparrow and infrared AIM-9 Sidewinder missiles for beyond-visual-range engagements, exposed the unreliability of early guided munitions in real combat scenarios. During the Vietnam War, missile hit probabilities hovered below 10% for AIM-7s and around 15% for AIM-9s due to factors like electronic countermeasures, launch envelope limitations, and environmental interference, forcing pilots into visual-range fights where the aircraft's lack of a fixed gun proved a liability. This necessitated external 20 mm cannon pods on early variants, which imposed drag penalties and restricted ammunition to 65 rounds, ultimately leading to the integration of an M61 Vulcan 20 mm rotary cannon in the F-4E starting in 1967, with 640 rounds stored internally.[96][84] The episode underscored the engineering imperative to retain kinetic backups in fighter designs, as missile technology maturation lagged behind tactical realities, influencing subsequent aircraft like the F-16 to prioritize internal guns alongside advanced sensors.[96] Aerodynamically, the F-4's configuration—low-mounted 45-degree swept wings with leading-edge slats for high-lift at low speeds, paired with an anhedral tail for lateral stability—optimized it for supersonic dash and carrier operations but yielded a wide turn radius of approximately 4,000 feet at Mach 0.9, prioritizing speed (Mach 2.23 maximum) over agility. Dihedral on wingtips and anhedral on the stabilators corrected pitch-up tendencies inherited from precursor designs like the F3H Demon, while high-mounted J79-GE-17 engines with afterburners delivered a thrust-to-weight ratio exceeding 1:1, enabling rapid acceleration to offset maneuverability deficits.[85][115] This balance highlighted the trade-off in multi-role fighters between interception performance and dogfighting, where excess power can compensate for geometric limitations, a principle echoed in later variable-geometry designs but affirming the value of empirical wind-tunnel and flight testing to quantify such compromises.[14] The aircraft's iterative "additive" engineering process, driven by Navy and Air Force requirements evolution, exemplified how incremental modifications—such as reinforced wings for bomb loads up to 18,000 pounds or avionics upgrades for pulse-Doppler radar in the F-4E—propagated changes across subsystems, increasing complexity and maintenance demands. Engine inlets were redesigned with variable ramps to manage supersonic airflow without boundary layer divergence, solving drag issues from fixed ramps, while the titanium central fuselage endured Mach 2+ skin temperatures up to 600°F.[115][14] These adaptations, spanning 1958 prototypes to 1979 production end, produced over 5,195 units and enabled role shifts from fleet defense to precision strikes, teaching that robust airframes with modular interfaces facilitate longevity but demand disciplined systems engineering to avoid cascading redesign costs.[14] Twin-engine redundancy proved critical for survivability, as the J79s' axial-flow design allowed single-engine returns from missions even under battle damage, with documented cases of Phantoms completing flights on one engine after flak hits.[116] However, the engines' high fuel consumption—up to 1,000 gallons per minute in full afterburner—necessitated large internal tanks (over 1,300 gallons) and aerial refueling booms, revealing the causal link between thrust demands and logistical burdens in sustained operations. This reinforced first-principles emphasis on propulsion efficiency in endurance-critical designs, influencing smokeless afterburner developments in successor engines like the F100.[85]Variants
[Variants - no content]Specifications (F-4E Variant)
The McDonnell Douglas F-4E Phantom II variant, introduced to address dogfighting deficiencies observed in earlier models, incorporated an internal M61A1 Vulcan 20 mm cannon and upgraded General Electric J79-GE-17 engines providing enhanced thrust.[30][38]General characteristics
- Crew: 2 (pilot and weapon systems officer)[117]
- Length: 63 ft 3 in (19.28 m)[117]
- Wingspan: 38 ft 5 in (11.7 m)[118]
- Height: 16 ft 6 in (5.0 m)[117]
- Wing area: 530 sq ft (49 m²)[118]
- Empty weight: 30,328 lb (13,757 kg)[118][119]
- Max takeoff weight: 61,795 lb (28,030 kg)[118][119][28]
- Powerplant: 2 × General Electric J79-GE-17A turbojets, 11,870 lbf (52.8 kN) thrust each dry; 17,900 lbf (79.6 kN) with afterburner[30][119]
Performance
- Maximum speed: Mach 2.2 (1,470 mph; 2,370 km/h) at 40,000 ft (12,000 m)[18]
- Cruise speed: 585 mph (940 km/h)[37]
- Combat range: 422 mi (680 km)[37]
- Ferry range: 1,615 mi (2,600 km) with drop tanks[37]
- Service ceiling: 60,000 ft (18,000 m)[18]
- Rate of climb: 30,000 ft/min (150 m/s)[18]
- Thrust/weight: 0.91 (loaded)[119]
Armament
- Guns: 1 × 20 mm M61A1 Vulcan cannon with 640 rounds[30]
- Hardpoints: 9 external pylons with capacity for up to 18,450 lb (8,400 kg) of ordnance, including AIM-7 Sparrow and AIM-9 Sidewinder missiles, Mk 82/83/84 bombs, AGM-65 Maverick, and nuclear weapons[120][38]
