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F-4 Phantom II

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F-4 Phantom II

F-4E from 347th TFW dropping 500-lb Mark 82 bombs

Type Fighter-bomber
Manufacturer McDonnell Aircraft/
McDonnell Douglas
Maiden flight 27 May 1958
Introduction 30 December 1960
Status 1,100 active in foreign service, and as drones, as of 2001
Primary users United States Air Force
United States Navy
United States Marine Corps
Produced 1958–1981
Number built 5,195
Unit cost US$2.4 million when new (F-4E)

The McDonnell Douglas F-4 Phantom II[1][2] is an American two-seat, twin-engined supersonic long-range all-weather fighter-bomber originally developed for the U.S. Navy by McDonnell Aircraft.[2]

The Phantom remained in production from 1958 to 1981, with a total of 5,195 built, and was used by the U.S. military from 1960 to 1996, serving with the U.S. Air Force, Marine Corps, and the US Navy.[3] It was used extensively by all three U.S. services operating in Vietnam, ending the war as the principal air superiority fighter for both the Navy and Air Force, as well as being important in the ground-attack and reconnaissance roles.[3]

The Phantom continued to form a major part of U.S. military air power throughout the 1970s and 80s, being gradually replaced by more modern aircraft such as the F-15 Eagle and F-16 Fighting Falcon in the U.S. Air Force and the F-14 Tomcat and F/A-18 Hornet in the U.S. Navy. It remained in service in the reconnaissance and Wild Weasel roles in the 1991 Gulf War.[4][5]

The Phantom was also operated by the armed forces of 11 other nations. Israeli Phantoms saw extensive combat in numerous Arab–Israeli conflicts, while Iran used its large fleet of Phantoms in the Iran–Iraq War. Phantoms remain in front line service with seven countries, and in use as an unmanned target in the U.S. Air Force.[6]

Overview

The F-4 Phantom was designed as a fleet defense fighter for the U.S. Navy, and first entered service in 1960. By 1963, it had been adopted by the U.S. Air Force for the fighter-bomber role. When production ended in 1981, 5,195 Phantom IIs had been built, making it the most numerous American supersonic military aircraft.[7] Until the advent of the F-15 Eagle, the F-4 also held a record for the longest continuous production with a run of 24 years. Innovations in the F-4 included an advanced pulse-doppler radar and extensive use of titanium in its airframe.[8]

Despite the imposing dimensions and a maximum takeoff weight of over 60,000 pounds (27,000 kg),[9] the F-4 had a top speed of Mach 2.23 and an initial climb of over 41,000 ft per minute (210 m/s).[10] Shortly after its introduction, the Phantom set 15 world records,[11] including an absolute speed record of 1,606.342 mph (2,585.086 km/h), and an absolute altitude record of 98,557 ft (30,040 m).[12] Although set in 1959–1962, five of the speed records were not broken until 1975.[11]

The F-4 could carry up to 18,650 pounds (8,480 kg) of weapons on nine external hardpoints, including air-to-air and air-to-ground missiles, and unguided, guided, and nuclear bombs.[13] Since the F-8 Crusader was to be used for close combat, the F-4 was designed, like other interceptors of the day, without an internal cannon;[14] In a dogfight, the RIO or WSO (commonly called "backseater" or "pitter") assisted in spotting opposing fighters, visually as well as on radar. It became the primary fighter-bomber of both the Navy and Air Force by the end of the Vietnam War.

Due to its distinctive appearance and widespread service with United States military and its allies, the F-4 is one of the best-known icons of the Cold War. It served in the Vietnam War and Arab–Israeli conflicts, with American F-4 crews achieving 277 aerial victories in South East Asia and completing countless ground attack sorties.[15]

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The Blue Angels fly their F-4Js abreast, for cross-country events.

The F-4 Phantom has the distinction of being the last United States fighter to attain ace status in the 20th century. During the Vietnam War, the USAF had one pilot and two WSOs,[16] and the USN one pilot and one RIO,[17] become aces in air-to-air combat. It was also a capable tactical reconnaissance and Wild Weasel (suppression of enemy air defenses) platform, seeing action as late as 1991, during Operation Desert Storm.[4][5]

The F-4 Phantom II was also the only aircraft used by both of the USA's flight demonstration teams.[18] The USAF Thunderbirds (F-4E) and the USN Blue Angels (F-4J) both switched to the Phantom for the 1969 season; the Thunderbirds flew it for five seasons,[19] the Blue Angels for six.[20]

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. The Phantom would be replaced by the F-15 Eagle and F-16 Fighting Falcon in the U.S. Air Force. In the U.S. Navy, it would be replaced by the F-14 Tomcat and the F/A-18 Hornet which revived the concept of a dual-role attack fighter.[21]

Design and development

Origins

The origins of McDonnell’s F-4 can be traced to a 1953 request by the Navy for an upgrade of the McDonnell F3H Demon carrier-borne fighter. Although the Vought F8U Crusader won the contract, the "Super Demon" (as McDonnell’s entrant was dubbed) was developed as a ground attack aircraft under the designation AH, which by 1955 had evolved into an all-weather air superiority fighter designated F4H. The F4H first flew in 1958 and remained in production from 1959 until 1981. Dave Lewis was the chief of preliminary design and, ultimately, the program manager for development and the sales effort.[22]

In 1952, McDonnell’s Chief of Aerodynamics, Dave Lewis, was appointed by CEO Jim McDonnell to be the company’s Preliminary Design Manager. 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. At the time, the Navy had separate fighter and attack branches, each with separate systems and operational requirements. After many iterations and various "enemy capability" assumptions, an unsolicited attack fighter was presented to the Navy. The McDonnell design called for two engines. The primary air-to-air armament was provided by the new Sparrow III air-to-air missiles, semi-recessed in the fuselage. The air-to-ground armament was to be as many bombs as could be carried on stations under the wings and aft of the Sparrows on the fuselage. No guns were offered. It took two years of hard work with the Bureau of Aeronautics and the Naval Air Warfare Division in the Pentagon, but the F-4 was sold with a configuration similar to what was originally proposed.[23]

Super Demon

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,[24] and variants powered by two Wright J65 engines, or two General Electric J79 engines.[25] The J79-powered version promised a top speed of Mach 1.97. On 19 September 1953, McDonnell approached the United States Navy with a proposal for the "Super Demon". Uniquely, the aircraft was to be modular—it could be fitted with one- or two-seat noses for different missions, with different nose cones to accommodate radar, photo cameras, four 20 millimeter 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 the supersonic fighter.[26]

The McDonnell design was therefore reworked into an all-weather fighter-bomber with 11 external hardpoints for weapons and on 18 October 1954, the company received a letter of intent for two YAH-1 prototypes. On 26 May 1955, four Navy officers arrived at the McDonnell offices and, within an hour, presented the company with an entirely new set of requirements. Because the Navy already had the 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.[2]

XF4H-1 prototype

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 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 degrees and was equipped with a boundary layer control system for better low-speed handling.[27]

Wind tunnel testing had revealed lateral instability requiring the addition of five degrees dihedral to the wings.[28] To avoid redesigning the titanium central section of the aircraft, McDonnell engineers angled up only the outer portions of the wings by 12 degrees which averaged to the required five degrees 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 degrees of anhedral to improve control at high angles of attack while still keeping the tailplane clear of the engine exhaust.[27] In addition, air intakes were equipped with movable ramps to regulate airflow to the engines at supersonic speeds. All-weather intercept capability was achieved thanks to the AN/APQ-50 radar. To accommodate carrier operations, the landing gear was designed to withstand landings with a sink rate of 23 ft per second (7 m/s), while the nose strut could extend by some 20 inches (50 cm) to increase angle of attack at takeoff.[28]

Naming the aircraft

There were proposals to name the F4H "Satan" and "Mithras", the Persian god of light.[29] In the end, the aircraft was given the less controversial name "Phantom II," the first "Phantom" being another McDonnell jet fighter, the FH-1. The Phantom II briefly carried the designation F-110A and was also given the name of "Spectre" by the USAF, neither title was used.[30]

Prototype testing

On 25 July 1955, the Navy ordered two XF4H-1 test aircraft and five YF4H-1 pre-production fighters. The Phantom made its maiden flight on 27 May 1958 with Robert C. Little at the controls. A hydraulic problem precluded 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 bleed air holes on each ramp; and the aircraft soon squared off against the XF8U-3. Due to operator workload, the Navy wanted a two-seat aircraft and on 17 December 1958 the F4H was declared a 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 pound-force (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 USS Independence.[28]

Production

Image:020906-f-9999r-006.jpg
A flight of USAF F-4Cs refuel from a KC-135 tanker before making a strike against targets in North Vietnam. The Phantoms are fully loaded with 750-pound general purpose bombs, Sparrow missiles and external fuel tanks.

Early in production, the radar was upgraded to a larger AN/APQ-72, necessitating the bulbous nose, and the canopy was reworked to improve visibility and make the rear cockpit less claustrophobic.[31] The Phantom underwent a great many changes during its career, summarized in the "Variants" section below.

The United States Air Force received Phantoms as the result of Robert McNamara’s push to create a unified fighter for all branches of the military. After an F-4B won the "Operation Highspeed" fly-off against the F-106 Delta Dart, the USAF borrowed two Naval F-4Bs, temporarily designating them F-110A "Spectre" in January 1962, and developed requirements for their own version. Unlike the Navy focus on interception, the USAF emphasized a 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.[32]

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), making it the second most produced and exported American military-jet; the F-86 Sabre still remains the most numerous jet-powered warplane produced and exported by the United States. Of these, 2,874 went to the USAF, 1,264 to the Navy and Marine Corps, and the rest to foreign customers.[18] The last U.S.-built F-4 went to Turkey, while the last F-4 ever built was completed in 1981 as an F-4EJ by Mitsubishi Heavy Industries in Japan. As of 2001, about 1,100 Phantoms remained in service worldwide, including QF-4 drones operated by the U.S. military.[33]

World records

To show off their new fighter, the Navy led a series of record-breaking flights early in Phantom development:[18]

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