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Northrop T-38 Talon

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The Northrop T-38 Talon is a two-seat, twinjet supersonic jet trainer designed and produced by the American aircraft manufacturer Northrop Corporation . It was the world's first supersonic trainer as well as the most produced.

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107-620: The T-38 can be traced back to 1952 and Northrop's N-102 Fang and N-156 fighter aircraft projects. During the mid-1950s, Northrop officials decided to adapt the N-156 to suit a recently issued general operating requirement by the United States Air Force (USAF) for a supersonic trainer to replace the Lockheed T-33 . The bid was successful, in no small part on its lower lifecycle cost comparisons to competing aircraft, and

214-436: A leading edge sweep of 45° and was equipped with blown flaps for better low-speed handling. Wind tunnel testing had revealed lateral instability, requiring the addition of 5° dihedral to the wings. 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

321-469: A Chinese MiG-17. The Phantom was then shot down, probably by an AIM-7 Sparrow from one of its wingmen. 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. On 17 June 1965, an F-4B from VF-21 Freelancers piloted by Commander Louis Page and Lieutenant John C. Smith shot down

428-548: A U.S. Navy-initiated refurbishment program called "Project Bee Line" 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. The USMC also operated

535-635: A combat radius of 400 mi (650 km). Northrop proposed the N-102 to meet the requirement, while other competitors were from Lockheed (the CL-246), North American Aviation (the NA-212) and Republic Aviation (the AP-55). The N-102 had a shoulder-mounted delta wing and a small all-moving tailplane mounted behind the wing. It would be powered by a single turbojet mounted in the lower aft fuselage which

642-569: 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. 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

749-515: A gun on the aircraft." 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

856-474: 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. On 10 July 1965, F-4Cs of the 45th TFS, 15th TFW, scored the USAF's first victories against North Vietnamese MiG-17s using AIM-9 Sidewinder air-to-air missiles. On 26 April 1966, an F-4C from the 480th Tactical Fighter Squadron scored

963-497: A relatively compact engine, around 400 lb installed weight, capable of 2,500 lb of thrust. Upon seeing the engine, Northrop VP-Engineering Edgar Schmued saw the possibility of reversing the trend toward the large fighters. Schmued and chief engineer Welko Gasich decided on a small, twin-engined "hot-rod" fighter, the N-156 . Northrop launched its N-156 project in 1954, aiming for a small, supersonic fighter jet capable of operating from

1070-498: 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; 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

1177-550: A somewhat unforgiving aircraft from an aerodynamic standpoint. The T-38 can be visually distinguished from both the F-5B and F-5F, which are also derived from the N-156, by the wings. The wing of the T-38 meets the fuselage straight and ends square, while the F-5 has leading edge extensions near the wing roots and wingtip launch rails for air-to-air missiles . The wings of both the T-38 and

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1284-544: A supersonic trainer, seeking to retire its 1940s-era Lockheed T-33s for an aircraft better suited to training pilots to fly its high speed fighter aircraft. Northrop officials decided to adapt the N-156 to this competition. The only other candidate was the two-seat version of the North American F-100 Super Sabre . Although the F-100 was not considered the ideal candidate for a training aircraft (it

1391-541: A total of 5,195 aircraft built, making it the most produced American supersonic military aircraft in history , and cementing its position as a signature combat aircraft of the Cold War . 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. The F-4, like other interceptors of its time,

1498-636: A variant powered by a Wright J67 engine, and variants powered by two Wright J65 engines, or two General Electric J79 engines. 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

1605-603: 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 . Proving highly adaptable, it entered service with the Navy in 1961 before it was adopted by the United States Marine Corps and the United States Air Force , and by the mid-1960s it had become a major part of their air arms. Phantom production ran from 1958 to 1981 with

1712-469: Is not capable of recovering from a spin), NAA was still considered the favorite in the competition due to that company's favored-contractor status with the USAF, but Northrop officials presented lifecycle cost comparisons that proved to be highly persuasive amongst USAF officials. Accordingly, Northrop was awarded an initial contract in June 1956 to produce three prototypes, designated YT-38 . On 10 April 1959,

1819-522: Is typically used to train its astronauts and as a chase plane . NASA's fleet is housed primarily at Ellington Field in Houston , Texas. NASA's internal projections showed the number of operational jet trainers falling to 16 by 2015. The agency spends $ 25–30 million annually to fly and maintain the T-38s. In 1966, two Project Gemini astronauts, Elliot See and Charles Bassett , died when their T-38 hit

1926-567: 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 December 2, President Bush reported that on 1 December, US fighter aircraft from Clark Air Base assisted Aquino repel a coup attempt. 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

2033-917: The Air Combat Command (ACC) and the Air Force Global Strike Command (AFGSC) retain T-38s as proficiency aircraft for U-2 pilots and B-2 pilots, respectively. The Air Training Command 's successor, the Air Education and Training Command (AETC), uses the T-38C to prepare pilots for the F-15C Eagle and F-15E Strike Eagle , the F-16 Fighting Falcon , B-52 Stratofortress , B-1B Lancer , B-2 Spirit , A-10 Thunderbolt , F-22 Raptor , and F-35 Lightning II . The AETC received T-38Cs in 2001 as part of

2140-772: 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 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

2247-454: 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. The "E" prefix was later dropped and

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2354-621: 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 F-4 Phantom II remained in use by the U.S. in the reconnaissance and Wild Weasel ( Suppression of Enemy Air Defenses ) roles in the 1991 Gulf War , finally leaving combat service in 1996. It was also the only aircraft used by both U.S. flight demonstration teams:

2461-668: The Islamic State group in the Middle East. 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. 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

2568-529: The Kowsar , had been constructed within Iran. The Northrop T-38 Talon is of a conventional configuration, with a small, low-mounted, long-chord wing, a single vertical stabilizer, and tricycle undercarriage . The cockpit accommodates a student pilot and instructor in a tandem seating arrangement. The flight controls were hydraulically -powered and lacked manual reversion, and thus the aircraft would be unflyable in

2675-494: The National Test Pilot School owns one T-38. Two others are in private ownership. More than 210 aircraft losses and ejections have been documented over the lifetime of the T-38. The USAF has recorded 149 fatalities since operations began in 1960. Data from General characteristics Performance Related development Related lists Northrop N-102 Fang The Northrop N-102 Fang

2782-472: The T-38A variant. The USAF had a small number of aircraft converted for weapons training, designated AT-38B , which were fitted with a gunsight and could carry a gun pod, rockets, or bombs on a centerline pylon. By the end of September 2017, 503 T-38s were still operational with the USAF, while many more remained in operation around the world. Most of the USAF's aircraft, T-38A and AT-38B, have been converted to

2889-793: The T-50 . Raytheon and Alenia Aermacchi offered the T-100 , an aircraft whose design originated with the M-346 . Boeing and Saab offered a new-technology design powered by the General Electric F404 turbofan engine. The Boeing/Saab bid first flew in December 2016. It was declared the winner of the T-X competition in September 2018. NASA operates a fleet of 32 T-38 trainers. The fleet

2996-696: 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. The operation was called off in the early stages of execution. The VMCJ-1 Golden Hawks (later VMAQ-1 and VMAQ-4 which had

3103-781: The United States Air Force Thunderbirds (F-4E) and the United States Navy Blue Angels (F-4J). 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 air forces of Iran , Greece , and Turkey . The aircraft has most recently been in service against

3210-712: 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. These were subsequently retired in 2004. The Marine Corps received its first F-4Bs in June 1962, with

3317-416: 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 ). 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

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3424-583: The ground-attack and aerial reconnaissance roles late in the war. During the Vietnam War, all five American servicemen who became aces  – one U.S. Air Force pilot, two weapon systems officers (WSOs), one U.S. Navy pilot and one radar intercept officer (RIO) – did so in F-4s. The F-4 continued to form a major part of U.S. military air power throughout the 1970s and 1980s, being gradually replaced by more modern aircraft such as

3531-881: 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. 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

3638-466: 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

3745-566: The Air Force officially ended use of the type. To show off their new fighter, the Navy led a series of record-breaking flights early in Phantom development: All in all, the Phantom set 16 world records. Five of the speed records remained unbeaten until the F-15 Eagle appeared in 1975. 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

3852-670: The Avionics Upgrade Program. The T-38Cs owned by the AETC have undergone propulsion modernization, which replaces major engine components to enhance reliability and maintainability, and an engine inlet/injector modification to increase available takeoff thrust. These upgrades and modifications, with the Pacer Classic program, were to extend the service life of T-38s past 2020. The T-38 has an availability goal of 75%, which it maintained in 2011. In 2015, its availability

3959-746: The Corps." VMFP-3 disestablished in August 1990 after the Advanced Tactical Airborne Reconnaissance System was introduced for the F/A-18D Hornet . 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

4066-556: The F-4 included an advanced pulse-Doppler radar and extensive use of titanium in its airframe. Despite imposing dimensions and a maximum takeoff weight of over 60,000 lb (27,000 kg), the F-4 has a top speed Mach 2.23 and an initial climb rate of over 41,000 ft/min (210 m/s). 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 . Like other interceptors of its day,

4173-412: The F-4 was designed without an internal cannon. 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. "Speed is life" was F-4 pilots' slogan, as the Phantom's greatest advantage in air combat was acceleration and thrust, which permitted

4280-638: 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). 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 . Phantoms would eventually equip numerous tactical fighter and tactical reconnaissance units in

4387-743: The F-4E. Note: Original amounts were in 1965 U.S. dollars. The figures in these tables have been adjusted for inflation to the current year. 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. The squadron completed carrier qualifications in October 1961 and Phantom's first full carrier deployment between August 1962 and March 1963 aboard Forrestal . The second deployable U.S. Atlantic Fleet squadron to receive F-4Bs

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4494-433: The F-5 family use conventional skin over spar-rib structure. The T-38's wings were originally designed to withstand 7.33-G loads and for a fatigue life of 4,000 flight hours. This proved sufficient for the majority of the training syllabus, but was a major limiting factor when the aircraft was used for aggressive dogfighting-style maneuvering. Incidents of wing tips separating mid-flight were reported. Northrop resolved this via

4601-582: The F4H " Satan " and " Mithras ". 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 and the Tri-Service aircraft designation system , F-4, was adopted in September 1962. Early in production, the radar was upgraded to

4708-461: 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 . There were proposals to name

4815-687: The N-156 was selected for the US Military Assistance Program and produced as the F-5 Freedom Fighter . Many of these have since reverted to a weapons-training role, as various air forces have introduced newer types into service. The F-5G was an advanced single-engined variant later renamed the F-20 Tigershark . In 2018, the Iranian Air Force announced that an outwardly similar aircraft, named

4922-631: The RF-4B with reconnaissance cameras with 46 built; 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. 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

5029-465: The T-38 and make it as easy to maintain as possible. To avoid removing the vertical fin while changing an engine, the fin was attached directly to the keel structure between the engines, and instead detaching the horizontal stabilizer along with the entire aft shell of the fuselage that surrounds the engines, which could be removed relatively easily via undoing several fasteners that hold the fuselage shell together and disconnecting two push rods that connect

5136-801: The T-38 have included the German Air Force , the Portuguese Air Force , the Republic of China Air Force , and the Turkish Air Force . During late 2010, the USAF launched the T-X program to procure a replacement for its T-38s. Bidders included a joint venture of BAE Systems and Rolls-Royce, offering the Hawk trainer , equipped with Rolls' Adour Mk951 engine with FADEC . Lockheed Martin and Korea Aerospace Industries , offered

5243-529: The T-38C through an avionics upgrade program. Improvements include the addition of a head-up display , global satellite positioning , inertial navigation system , and traffic collision avoidance system . Most aircraft have received a propulsion modification to improve low-altitude engine thrust. Around a third of the fleet, those that experience more severe usage, are currently undergoing structural replacements and upgrades, as well as receiving new wings, to extend their service life to 2029. The fighter version of

5350-412: The US Navy for dissimilar air combat training until replaced by the similar Northrop F-5 Tiger II . Pilots of other NATO nations have commonly flown the T-38 during joint training programs with American pilots. The T-38 remains in service as of 2023 with several air forces. As of 2023, the T-38 has been in service for over 60 years with the USAF, its original operator. In September 2018, USAF announced

5457-410: The US Navy's escort carriers . When the Navy chose not to pursue equipping its fleets in such a fashion, favoring large fleet carriers instead, Northrop opted to continue work on the N-156 using in-house funding. It was instead recast as a lightweight fighter, referred to as the N-156F , that was primarily aimed at the export market. In the mid-1950s, the USAF issued a general operating requirement for

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5564-540: 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. The F-4J improved both air-to-air and ground-attack capability; deliveries begun in 1966 and ended in 1972 with 522 built. It

5671-455: The USAF active, ANG, and Air Force Reserve (AFRES). 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. In early December 1989, USAF F-4s, from Clark Air Base , participated in Operation Classic Resolve, President Bush's response to

5778-399: The USAF's first F-4Cs in January 1964, achieving initial operational capability (IOC) in October 1964. 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. Unlike the U.S. Navy and U.S. Marine Corps, which flew the Phantom with a Naval Aviator (pilot) in

5885-426: The USAF, 1,264 to the Navy and Marine Corps, and the rest to foreign customers. 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. As of 2008, 631 Phantoms were in service worldwide, while the Phantoms were in use as a target drone (specifically QF-4Cs) operated by the U.S. military until 21 December 2016, when

5992-431: The USMC. They soon began close air support missions (CAS) and VMFA-314, VMFA-232 Red Devils , VMFA-323 Death Rattlers and VMFA-542 Bengals soon arrived at the primitive airfield. 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. Marine Phantoms from VMFA-323 and VMFA-531 operating from

6099-595: 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 . 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. The USN and USMC received

6206-405: The Wright J67 (a license-built Bristol Olympus ) or the General Electric J79 , with all of the engines giving an estimated speed of at least Mach 2. In early 1953, the USAF selected Lockheed's CL-246, which became the Lockheed F-104 Starfighter , but Northrop at first continued work on the N-102 with the hope of gaining export orders, building a mock-up of the aircraft in USAF colors. However,

6313-510: 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. 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

6420-449: 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. Peak numbers of combat F-4s occurred in 1972, when 353 were based in Thailand. 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). The RF-4C

6527-439: The aircraft. Two decades after the aircraft entered service this was solved on the F-4S, which was fitted with the −10A engine variant with a smokeless combustor . 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

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6634-400: The catapult portion of a takeoff. 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

6741-495: The central keel. This design enabled ground crews to remove and replace an engine in roughly one hour. The USAF Strategic Air Command (SAC) had T-38s in service from 1978 until SAC's 1991 inactivation. These aircraft were used to enhance the career development of bomber and tanker copilots through the Accelerated Copilot Enrichment Program. They were later used as proficiency aircraft for all B-52 , B-1 , Lockheed SR-71 , U-2 , Boeing KC-135 , and KC-10 pilots. SAC's successors,

6848-761: 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. 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

6955-435: 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

7062-462: The company received an initial order to build three prototypes. The first of these, designated YT-38 , made its maiden flight on 10 April 1959. The T-38 was introduced to USAF service on 17 March 1961. The USAF is the largest operator of the T-38. Additional operators of the T-38 include NASA and the United States Navy . U.S. Naval Test Pilot School in Patuxent River, Maryland, is the principal US Navy operator. Other T-38s were previously used by

7169-399: The design team headed by Welko E. Gasich, Northrop's Chief of Advanced Design. On 12 December that year, the United States Air Force (USAF) issued a requirement for a lightweight air superiority aircraft to replace the F-100 supersonic fighter. The new aircraft was expected to enter service in 1957 and was required to have a speed of at least Mach 1.3 at 35,000 ft (11,000 m) and

7276-440: 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. 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

7383-402: 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

7490-436: The event of both engines failing mid-flight. Its handling was relatively conventional and viceless. While it was originally considered to be too easy to fly compared with frontline fighters of the 1960s, by the twenty-first century, it had become regarded as the most challenging aircraft in the USAF's inventory. The aircraft's nimble performance earned it the nickname "white rocket". It had been considered by trainee pilots to be

7597-411: The few armed flying forces using dedicated supersonic final trainers, as most, such as the US Navy, use high-subsonic trainers. During 1962, the T-38 set absolute time-to-climb records for 3,000, 6,000, 9,000, and 12,000 meters, beating the records for those altitudes set by the F-104 in December 1958. The F-4 Phantom beat the T-38's records less than a month later. The majority of T-38s built were of

7704-416: The first North Vietnamese MiG of the war. 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

7811-723: The first Phantom combat sortie of the Vietnam War on 5 August 1964, flying bomber escort in Operation Pierce Arrow . 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. 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

7918-535: The first YT-38 performed its maiden flight at the hands of test pilot Lew Nelson . The type was quickly adopted. The first production examples were delivered in 1961, entering service on 17 March 1961, complementing the Cessna T-37 Tweet primary jet trainer. When production ended in 1972, 1,187 T-38s had been built, plus two N-156T prototypes. Since its introduction, an estimated 50,000 military pilots have trained on this aircraft. The USAF remains one of

8025-428: The first aerial victory by a U.S. aircrew over a North Vietnamese MiG-21 "Fishbed" . 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

8132-600: The first definitive Phantom, the F-4B which was equipped with the Westinghouse APQ-72 radar (pulse only), a Texas Instruments 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

8239-607: The first examples at NAS Miramar . 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

8346-466: 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; 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

8453-457: The fuselage to exert less drag and produce fewer aerodynamic disturbances. The J85-5A engine, despite generating up to 3,850 lb of static thrust, was relatively compact and lightweight for the era, weighing less than 600 pounds. Air was supplied to the engines via intakes at the wing roots . A twin-engine arrangement had been pursued to provide a greater margin of safety. Various design decisions were taken and features were incorporated to simplify

8560-872: The hazardous post-strike reconnaissance missions. The USAF Thunderbirds used the F-4E from the 1969 season until 1974. 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

8667-473: 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

8774-527: The installation of new wings with thickened skins. Throughout the development process, a strict weight control regime was exercised by the design team. This was one reason for the T-38's relative simplicity; only basic systems for navigation and communication were provided. No fuel was housed within the wings while no provision for external stores was made. The aircraft's twin General Electric J85-5A turbojet engines were accommodated within

8881-498: 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

8988-472: The lightweight fighter concept would ultimately come to fruition with the F-5 Freedom Fighter , itself spawning a moderately successful fighter family. In the early 1950s, concerns grew in the United States about the growing weight, complexity and cost of modern fighter aircraft, and in late 1952, Northrop started a design study for a simple, lightweight, supersonic fighter aircraft, the N-102 Fang, with

9095-456: 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. The McDonnell design was therefore reworked into an all-weather fighter-bomber with 11 external hardpoints for weapons and on 18 October 1954,

9202-490: 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. 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

9309-411: The pilot's control stick to the horizontal stabilizer's hydraulic actuators. To avoid having to break and reconnect multiple hydraulic lines during an engine swap, designers mounted the hydraulic pump and other accessory drives on the fuselage which joined to the engine by a short driveshaft . Several internal check valves prevented a loss of hydraulic fluid. The engines hung from rails on either side of

9416-476: 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

9523-575: The reliability and safety margin. The J85-powered design studies eventually formed the basis of the F-5 fighter family. The design was the subject of a 1957 design patent . Data from Northrop N-102 "Fang" General characteristics Performance Armament Related development Aircraft of comparable role, configuration, and era [REDACTED] Media related to N-102 Fang at Wikimedia Commons McDonnell Douglas F-4 Phantom II The McDonnell Douglas F-4 Phantom II

9630-656: The replacement of the Talon by the Boeing–Saab T-7 Red Hawk with phaseout to begin in 2023. In 1952, Northrop began work on a fighter project, the N-102 Fang , with shoulder-mounted delta wing and a single engine. The proposed General Electric J79 engine, weighing nearly two tons, meant the resulting aircraft would be large and expensive. During 1953, representatives from General Electric Aviation 's newly created Small Aircraft Engine Department showed Northrop

9737-463: 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. 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

9844-720: The roof of a McDonnell Douglas fabrication building at Lambert Field in St. Louis. Visibility was poor, but a later investigation concluded that the cause of the crash was likely pilot error. During the Space Shuttle era, an established NASA tradition was for astronauts to arrive at the Kennedy Space Center in T-38 Talons. Seven privately owned T-38s are in the U.S. Boeing owns two T-38s, which are used as chase planes. Thornton Corporation owns two T-38s, and

9951-652: 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. In USAF service, the F-4 was initially designated the F-110A prior to the introduction of

10058-470: The throttles and air speed during landing attempts. Despite these factors, the T-38 has been regarded as a relatively safe trainer aircraft even into the twenty-first century. Between 1961 and 2005, the fleet has cumulatively flown 25 million hours, during which 150 of the 1,187 T-38s built between 1961 and 1972 were recorded as lost, resulting in 45 deaths. Besides the USAF and the USN, other military operators of

10165-418: The use of a single, large engine meant that the aircraft could not be as light or cheap as Northrop wanted, and Northrop stopped work on the N-102 during 1954. Northrop continued work on lightweight fighters, basing its further studies on the use of two small General Electric J85 engines, which allowed a much lighter and cheaper aircraft, with Northrop's design team believing that twin engines would increase

10272-402: The war. On 9 September 1972, WSO Capt Charles B. DeBellevue became the highest-scoring American ace of the war with six victories. and WSO Capt Jeffrey Feinstein became the last USAF ace of the war on 13 October 1972. 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

10379-770: Was 60%. After graduating from basic flying on the Cessna T-37 Tweet , pilots were trained on more advanced aspects, including supersonic flight, blind flying, formation flight, handling stalls , single-engine flight procedures, low speed flight, and landing techniques. Prior to the USAF ceasing the practice of trainees flying within icy conditions, the T-38's engines were prone to being damaged by ingesting ice. The relatively small engine intakes are also known to be problematic when flown at low speeds under 'hot and high' conditions. The landing gear's brakes have been criticised for being relatively weak, one of several factors that necessitates care while landing. Several incidents, including fatalities, have occurred due to imprecise management of

10486-559: Was a fighter aircraft design created by Northrop Corporation and proposed to the United States Air Force in 1953. The Fang was explicitly designed as a ”light” or “lightweight fighter” in direct response to what Northrop saw as the ever-increasing weight, size, complexity, and cost of Western fighter designs. While the Fang was ultimately overlooked in-favor of the Lockheed F-104 Starfighter , Northrop’s interest in

10593-538: Was added to operate the powerful radar; designers believed that air combat in the next war would overload solo pilots with information. 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

10700-658: 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), a new integrated missile control system and the AN/AJB-7 bombing system for expanded ground attack capability. The F-4N (updated F-4Bs) with smokeless engines and F-4J aerodynamic improvements started in 1972 under

10807-563: Was flown by Maj Mike Webb and Maj Gary Leeder of the Idaho ANG. 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. Replacing the QF-106, the QF-4 program achieved IOC in 1997, with the last QF-106 being shot down on 20 February 1997. It was expected that

10914-501: Was initially designed without an internal cannon. Some later models incorporated an internal M61 Vulcan rotary cannon. Beginning in 1959, it set 15 world records for in-flight performance, including an absolute speed record and an absolute altitude record. The F-4 was used extensively during the Vietnam War . It served as the principal air superiority fighter for the U.S. Air Force, Navy, and Marine Corps and became important in

11021-578: 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. The last operational USAF/ANG F-4 to land

11128-476: Was operated by four squadrons, and of the 83 losses, 72 were in combat including 38 over North Vietnam (seven to SAMs and 65 to AAA). 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. On 28 August 1972, Captain Steve Ritchie became the first USAF ace of

11235-603: Was supplied by air from a variable-geometry ventral air inlet. This promised smoother, more efficient airflow to the engine at the risk of being more vulnerable to ingestion of foreign objects and damage to the engine. A number of different engines were proposed, including the Pratt & Whitney J57 , the Wright J65 (a license-produced derivative of the British Armstrong Siddeley Sapphire ),

11342-632: Was the VF-102 Diamondbacks , who promptly took their new aircraft on the shakedown cruise of Enterprise . 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 . By the time of the Tonkin Gulf incident , 13 of 31 deployable navy squadrons were armed with the type. F-4Bs from Constellation made

11449-487: Was the only aircraft in the USAF inventory equipped for the Suppression of Enemy Air Defenses (SEAD) 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

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