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The AIDC F-CK-1 Ching-Kuo ( Chinese : 經國號戰機 ; pinyin : Jīngguó Hào Zhànjī ), commonly known as the Indigenous Defense Fighter ( IDF ), is a multirole combat aircraft named after Chiang Ching-kuo , the late President of the Republic of China . The aircraft made its first flight in 1989. It entered service with Republic of China Air Force (Taiwan) in 1992. All 130 production aircraft were manufactured by 1999.

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83-565: (Redirected from CK1 ) Ck1 or CK1 may refer to: Transportation AIDC F-CK-1 Ching-kuo , the Taiwanese fighter jet the F-16 variant, see F-16 Fighting Falcon variants Chang Kong CK-1 , the radio-controlled target drone Cicaré CK.1 , the Argentine helicopter the locomotive, see CK class Biochemistry Keratin 1

166-569: A boxcar . Similarly, their pilots were given less training in combat maneuvers, and more in radio-directed pursuit. The Soviets' main interceptor was initially the Su-9 , which was followed by the Su-15 and the MiG-25 "Foxbat". The auxiliary Tu-128 , an area range interceptor, was notably the heaviest fighter aircraft ever to see service in the world. The latest and most advanced interceptor aircraft in

249-485: A brief period of time they fared rapid development in both speed, range, and altitude. At the end of the 1960s, a nuclear attack became unstoppable with the introduction of ballistic missiles capable of approaching from outside the atmosphere at speeds as high as 3 to 4 miles per second (5 to 7 km/s). The doctrine of mutually assured destruction replaced the trend of defense strengthening, making interceptors less strategically logical. The utility of interceptors waned as

332-462: A chosen aspect of performance. A "point defense interceptor" is of a lightweight design, intended to spend most of its time on the ground located at the defended target, and able to launch on demand, climb to altitude, manoeuvre and then attack the bomber in a very short time, before the bomber can deploy its weapons. At the end of Second World War, the Luftwaffe ' s most critical requirement

415-459: A command centre in the Horse Guards building. The Pup proved to have too low performance to easily intercept Gotha G.IV bombers, and the superior Sopwith Camels supplanted them. The term "interceptor" was in use by 1929. Through the 1930s, bomber aircraft speeds increased so much that conventional interceptor tactics appeared impossible. Visual and acoustic detection from the ground had

498-514: A larger antenna than used by the F-20. and this adaptation resulted in the look-down and shoot-down capability of GD-53 being greatly enhanced in comparison to that of the original AN/APG-67 , reaching that of the AN/APG-66 . The radar can simultaneously track 10 targets and engage two of the 10 targets tracked with TC-2 active radar seeker BVRAAMs. The design is inherently unstable in pitch, so

581-472: A much larger area from attack, depending on greater detection capabilities, both in the aircraft themselves and operating with AWACS, rather than high speed to reach targets. The exemplar of this concept was the Tupolev Tu-28 . The later Panavia Tornado ADV was able to achieve long range in a smaller airframe through the use of more efficient engines. Rather than focusing on acceleration and climb rate,

664-694: A pair of proposals for interceptor aircraft, the first such designation in the US. One proposal was for a single-engine fighter, the other for a twin-engine. Both were required to reach an altitude of 20,000 feet (6,100 m) in six minutes as a defense against bomber attack. Kelsey said later that he used the interceptor designation to sidestep a hard USAAC policy restricting fighters to 500 pounds (230 kg) of armament. He wished for at least 1,000 pounds (450 kg) of armament so that American fighters could dominate their battles against all opponents, fighters included. The two aircraft resulting from these proposals were

747-510: A range of only a few miles, which meant that an interceptor would have insufficient time to climb to altitude before the bombers reached their targets. Standing combat air patrols were possible but only at great cost. The conclusion at the time was that " the bomber will always get through ". The invention of radar made possible early, long-range detection of aircraft on the order of 100 miles (160 km), both day and night and in all weather. A typical bomber might take twenty minutes to cross

830-701: A simplified version of the IDF for LIFT, and that such a concept could have a cost as low as US$ 16 million per unit, compared to the T-50's 19 million. However, the F-CK-1 LIFT modifications or new production concepts never received government funding or approval. In May 2006, Lt. General Cheng Shih-Yu testified that the MND indeed plans to retire the F-5E/F by 2010 and allow the in-service IDFs to take over training missions. It

913-619: A step and roughly doubled operational altitudes. Although radars also improved in performance, the gap between offense and defense was dramatically reduced. Large attacks could so confuse the defense's ability to communicate with pilots that the classic method of manual ground controlled interception was increasingly seen as inadequate. In the United States, this led to the introduction of the Semi-Automatic Ground Environment to computerize this task, while in

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996-545: A two-seater. The first successful test flight by single-seater FSD A1 was made on May 28, 1989. The two-seater FSD B1 conducted its first flight on July 10, 1990. Production of ten pre-production units began in October 1990. The first four were delivered in March 1992 and the last in 1993. Mechanical defects caused two crashes, one in 1991 and one in 1993, during pre-production. The ROCAF's initial order for 256 aircraft

1079-453: A very high fuel consumption. This led fighter prototypes emphasizing acceleration and operational ceiling, with a sacrifice on the loiter time, essentially limiting them to point defense role. Such were the mixed jet/rocket power Republic XF-91 or Saunders Roe SR.53 . The Soviet and Western trials with zero-length launch were also related. None of these found practical use. Designs that depended solely on jet engines achieved more success with

1162-605: Is a type of fighter aircraft designed specifically for the defensive interception role against an attacking enemy aircraft, particularly bombers and reconnaissance aircraft . Aircraft that are capable of being or are employed as both "standard" air superiority fighters and as interceptors are sometimes known as fighter-interceptors . There are two general classes of interceptor: light fighters , designed for high performance over short range; and heavy fighters , which are intended to operate over longer ranges , in contested airspace and adverse meteorological conditions . While

1245-678: Is only that company's operational planning concept. The Ministry of National Defense and the Air Force currently do not have such a plan". The letter then said that due to a tight budget allocation the ROCAF would instead ask AIDC to extend the life of the AT-3 and continue to use the F-5 in the LIFT role. In 2003, the former AIDC Chairman Huang Jung-Te said that AIDC still hoped the ROCAF would consider using

1328-446: Is that interceptors often look very impressive on paper, typically outrunning, outclimbing and outgunning slower fighter designs. However, pure interceptors fare poorly in fighter-to-fighter combat against the same "less capable" designs due to limited maneuverability especially at low altitudes and speeds. In the spectrum of various interceptors, one design approach especially shows sacrifices necessary to achieve decisive benefit in

1411-544: Is unclear what modifications (if any) will be made to IDFs after they become trainers. The trainers produced by the program would later named AIDC T-5 Brave Eagle , and four prototypes were rolled out in 2019. Data from GlobalSecurity.org Milavia, TaiwanAirPower.org General characteristics Performance Armament Avionics Related development Aircraft of comparable role, configuration, and era Related lists Interceptor aircraft An interceptor aircraft , or simply interceptor ,

1494-645: The Convair F-106 Delta Dart , Sukhoi Su-15 , and English Electric Lightning . Through the 1960s and 1970s, the rapid improvements in design led to most air-superiority and multirole fighters , such as the Grumman F-14 Tomcat and McDonnell Douglas F-15 Eagle , having the performance to take on the point defense interception role, and the strategic threat moved from bombers to intercontinental ballistic missiles (ICBMs). Dedicated interceptor designs became increasingly rare, with

1577-601: The F-104 Starfighter (initial A version) and the English Electric Lightning . The role of crewed point defense designs was reassigned to uncrewed interceptors— surface-to-air missiles (SAMs)—which first reached an adequate level in 1954–1957. SAM advancements ended the concept of massed high-altitude bomber operations, in favor of penetrators (and later cruise missiles ) flying a combination of techniques colloquially known as "flying below

1660-627: The F-86D and F-89 Scorpion . In the late 1940s ADC started a project to build a much more advanced interceptor under the 1954 interceptor effort, which eventually delivered the F-106 Delta Dart after a lengthy development process. Further replacements were studied, notably the NR-349 proposal during the 1960s, but came to nothing as the USSR strengthened their strategic force with ICBMs. Hence,

1743-554: The Messerschmitt Me 163 Komet , which was the only rocket-powered, crewed military aircraft to see combat. To a lesser degree, the Mikoyan-Gurevich MiG-15 , which had heavy armament specifically intended for anti-bomber missions, was also a specialized day interceptor. Night fighters and bomber destroyers are interceptors of the heavy type, although initially they were rarely referred to as such. In

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1826-568: The Taiwanese nuclear weapons then in development. The primary delivery method was to be the Sky Horse missile. Weapons designers at CSIST were instructed to design the nuclear weapon to fit within the dimensions of the F-CK-1's centerline drop tank (~50 cm diameter). Modifications to the aircraft would have been required for it to obtain the desired 1,000 km range (especially without

1909-713: The Tien Chien 2 (TC-2) is an active radar homing Beyond Visual Range missile . The first test firing of the TC-1 missile was performed by an F-5E in April 1986, with the Beech target drone successfully destroyed. Initial production of the TC-1 began in 1989, and it entered service in 1991. Both the AIM-9 and the TC-1 have been seen in use on operational IDFs. CSIST is believed to have cooperated with Motorola and Raytheon on

1992-551: The United States refused to sell them F-20 Tigershark and F-16 Fighting Falcon jet fighters following diplomatic pressure from China . Taiwan therefore decided to develop an advanced indigenous jet fighter. The Aerospace Industrial Development Corporation (AIDC), based in Taichung , Taiwan , designed and built the IDF jet fighter. The preliminary search for a replacement for the ROCAF's F-5s and F-104s began with

2075-745: The XA-3 Lei Ming single seat attack aircraft, due to the believed high risks of the XF-6 project. The signing of the 1982 US-China Joint Communiqué limited arms sales to Taiwan. The United States refused to sell the General Dynamics F-16 Fighting Falcon and the Northrop F-20 Tigershark (which had been developed largely to meet Taiwanese national defense needs for an advanced jet fighter to replace their older F-5 jet fighters ) thereby ensuring

2158-528: The XF-6 indigenous fighter project, later renamed Ying Yang , in the late 1970s. After the US established formal relations with China and ended the Mutual Defense Treaty with Taiwan , President Chiang Ching-Kuo decided to expand the indigenous defense industry and on August 28, 1980, ordered AIDC to design an indigenous interceptor . Originally, the ROCAF listed the priority of the XF-6 behind

2241-519: The Calvin Klein product, see Calvin Klein (company) Pentecost biogeographic region, see Interim Biogeographic Regionalisation for Australia [REDACTED] Topics referred to by the same term This disambiguation page lists articles associated with the same title formed as a letter–number combination. If an internal link led you here, you may wish to change the link to point directly to

2324-598: The Crested Goshawk. As of 12/2009, 71 F-CK-1 A/B are upgrading to F-CK-1 C/D over 4 years span for over US$ 500 million, according to AIDC CEO, under Project Hsiang Chan (翔展), as AIDC and ROCAF had signed a contract for the expected upgrade program. In 2018 AIDC delivered the last upgraded F-CK-1 C/D to the Republic of China Air Force. According to the media, the AIDC IDF trainer concept apparently involved

2407-476: The F-106 ended up serving as the primary USAF interceptor into the 1980s. As the F-106 was retired, intercept missions were assigned to the contemporary F-15 and F-16 fighters, among their other roles. The F-16, however, was originally designed for air superiority while evolving into a versatile multirole fighter. The F-15, with its Mach 2.5 maximum speed enabling it to intercept the fastest enemy aircraft (namely

2490-579: The IDF could supercruise with the new engine. At the same time, General Electric Aviation decided to enter the market with the J101/SF, a smaller version of the F404. However, after the IDF order was cut in half due to budget concerns, the TFE1088-12 engine upgrade plan ended as well. The cooperation between AIDC and General Dynamics (GD) was divided into four phases: GD's assistance was restricted by

2573-546: The IDF development project in May 1982 following the ROCAF's failure to purchase new fighters from the United States as a result of Chinese diplomatic pressure. The project, led by Hsi-Chun Mike Hua , later known as the father of the Indigenous Defense Fighter , was named An-Hsiang (安翔, Safe Flight) and divided into four sections in 1983: In April 1997 American company Litton's Applied Technology division

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2656-480: The IDF incorporated a modern triple-redundant full authority fly-by-wire control system. The avionics suite was based on modular architecture with dual redundant MIL-STD-1553B digital databuses. The Honeywell H423 inertial navigation system , the TWS-95 RHAWS, and a Bendix-King head-up display were selected. Some capabilities may have been delayed or dropped in order to meet the performance requirement, since

2739-444: The IDF to carry an additional 771 kg of fuel. In addition, it includes an improved avionics suite, retrofitted electronic warfare capabilities, and new weapons systems. The landing gear has been strengthened to accommodate the additional payload and fuel, but the plan for a dielectric radar-absorbing "stealth" fuselage was dropped due to concerns over weight. The project consists of three phases: The development contract for

2822-750: The McDonnell Douglas F-4 Phantom as its primary interceptor from the mid-1970s, with the air defence variant (ADV) of the Panavia Tornado being introduced in the 1980s. The Tornado was eventually replaced with a multirole design, the Eurofighter Typhoon . The Shenyang J-8 is a high-speed, high-altitude Chinese-built single-seat interceptor. Initially designed in the early 1960s to counter US-built B-58 Hustler bombers, F-105 Thunderchief fighter-bombers and Lockheed U-2 reconnaissance planes, it still retains

2905-669: The MiG-25 Foxbat), is also not a pure interceptor as it has exceptional agility for dogfighting based upon the lessons learned from Vietnam; the F-15E Strike Eagle variant adds air interdiction while retaining the interception and air-to-air combat of other F-15s. Presently, the F-22 is the USA's latest combat aircraft that serves in part as an interceptor due to its Mach 2+ speed as well as supercruise capabilities, however it

2988-673: The Soviet (now Russian) inventory is the MiG-31 "Foxhound". Improving on some of the flaws on the proceeding MiG-25, the MiG-31 has better low altitude and low speed performance, in addition to carrying an internal cannon. Russia, despite merging the PVO into the VVS, continues to maintain its dedicated MiG-31 interceptor fleet. In 1937, USAAC lieutenants Gordon P. Saville and Benjamin S. Kelsey devised

3071-532: The TC-2's active seeker, which is believed to be based on their seeker design which was proposed for the AIM-120. 40 pre-production TC-2 missiles were produced before 1995, and were the only BVR AAMs that the ROCAF had in its inventory during the 1995–96 Taiwan Strait Missile Crisis . Over 200 production TC-2s were originally planned. During the F-CK-1's development, it was tapped as the secondary delivery vehicle for

3154-608: The TFE1042-7 for the AMX or the F-5 upgrade. AIDC also suggested upgrading the TFE1042-7 to 8,000 lbf (36 kN) thrust in a twin-engine installation, in order to compete with the GE F404. However, the JAS 39 Gripen project decided to continue with a single F404, and Piaggio asked to participate at a later date due to financial concerns. ITEC completely redesigned the TFE1042-7 into

3237-593: The TFE1042-70 ;– for example, the bypass ratio was changed from 0.84 to 0.4, and the investment had increased from US$ 180 million to about US$ 320 million. However, to avoid pressures from China, the US government had asked all American companies cooperating with the Taiwan on the IDF project to remain low-key. Therefore, the perception that "the TFE1042 is merely the civilian engine TFE731 with an afterburner"

3320-462: The UK it led to enormously powerful radars to improve detection time. The introduction of the first useful surface to air missiles in the 1950s obviated the need for fast reaction time interceptors as the missile could launch almost instantly. Air forces increasingly turned to much larger interceptor designs, with enough fuel for longer endurance, leaving the point-defense role to the missiles. This led to

3403-588: The US State Department's arms export control, which limited GD's work to initial design consulting but not further development, production, or marketing. Many different airframe design concepts were explored (e.g. the 2D Thrust-Vectoring nozzle of XX-201, the double delta wings/twin tailed 401). After the General Electric J79 was officially abandoned as the potential engine solution in 1983, three configurations emerged from AIDC. At

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3486-599: The abandonment of a number of short-range designs like the Avro Arrow and Convair F-102 in favor of much larger and longer-ranged designs like the North American F-108 and MiG-25 . In the 1950s and 1960’s during the Cold War , a strong interceptor force was crucial for the opposing superpowers as it was the best means to defend against an unexpected nuclear attack by strategic bombers . Hence, for

3569-470: The ability to 'sprint' at Mach 2+ speeds, and later versions can carry medium-range PL-12/SD-10 MRAAM missiles for interception purposes. The PLAAF/PLANAF currently still operates approximately 300 or so J-8s of various configurations. Several other countries also introduced interceptor designs, although in the 1950s–1960s several planned interceptors never came to fruition, with the expectation that missiles would replace bombers. The Argentine FMA I.Ae. 37

3652-458: The aircraft themselves. They were first to introduce all-weather avionics , assuring successful operations during night, rain, snow, or fog. Countries that were strategically dependent on surface fleet, most notably US and UK, maintained also fleet defense fighters , such as the F-14 Tomcat . During the Cold War , an entire military service, not just an arm of the pre-existing air force,

3735-697: The bombing raids. Rocket-boosted variants of both of Germany's jet fighters; the Me 262 in its "C" subtype series, all nicknamed "home protector" ( Heimatschützer , in four differing formats) and the planned He 162 E subtype, using one of the same BMW 003R turbojet/rocket "mixed-power" engine as the Me 262C-2b Heimatschützer II , but were never produced in quantity. In the initial stage of Cold War , bombers were expected to attack flying higher and faster, even at transonic speeds. Initial transonic and supersonic fighters had modest internal fuel tanks in their slim fuselages, but

3818-409: The centerline drop tank available) and were envisioned to include more efficient non-afterburning engines. The F-CK-1 would not have been able to fulfill the nuclear strike mission until mid-1989 at the very earliest. Early designs called for an unpowered gravity bomb . The nuclear weapons program was shut down under US pressure before the F-CK-1 entered service and the dedicated nuclear strike variant

3901-432: The continuation of the indigenous fighter project. Although US President Ronald Reagan reluctantly accepted his advisers' suggestion of building relations with China to counter the USSR, Reagan decided to balance the 1982 US-PRC Communiqué with the " Six Assurances " to Taiwan. This opened the door for US technology transfer and assistance to Taiwan's defense industry, including the IDF project. The AIDC officially began

3984-481: The cytokeratin, see Type II keratin Casein kinase 1 , a family of protein kinases Asteroids 1994 CK1, see 10146 Mukaitadashi 1993 CK1, see 20043 Ellenmacarthur 1989 CK1, see 4836 Medon 1986 CK1, see 3951 Zichichi 1983 CK1, see 4198 Panthera Other Crusader Kings I , a grand strategy computer game by Paradox Interactive the illicit drug cocktail, see cocaine and ketamine

4067-631: The defending fighters. The Me 163 required an airbase, however, which were soon under constant attack. Following the Emergency Fighter Program , the Germans developed even odder designs, such as the Bachem Ba 349 Natter , which launched vertically and thus eliminated the need for an airbase. In general all these initial German designs proved difficult to operate, often becoming death traps for their pilots, and had little effect on

4150-458: The design emphasis is on range and missile carrying capacity, which together translate into combat endurance, look-down/shoot-down radars good enough to detect and track fast moving interdictors against ground clutter , and the capability to provide guidance to air-to-air missiles (AAM) against these targets. High speed and acceleration was put into long-range and medium-range AAMs, and agility into short range dog fighting AAMs, rather than into

4233-464: The detection zone of early radar systems, time enough for interceptor fighters to start up, climb to altitude and engage the bombers. Ground controlled interception required constant contact between the interceptor and the ground until the bombers became visible to the pilots and nationwide networks like the Dowding system were built in the late 1930s to coordinate these efforts. During World War II

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4316-540: The early Cold War era the combination of jet -powered bombers and nuclear weapons created air force demand for highly capable interceptors; it is in regards to this period that the term is perhaps most recognized and used. Cold War-era interceptors became increasingly distinct from their air superiority counterparts, with the former often sacrificing range, endurance, and maneuverability for speed, rate of climb , and armament dedicated to attacking large strategic bombers . Examples of classic interceptors of this era include

4399-405: The effectiveness of interceptor aircraft meant that bombers often needed to be escorted by long range fighter aircraft. Many aircraft were able to be fitted with Aircraft interception radar , further facilitating the interception of enemy aircraft. The introduction of jet power increased flight speeds from around 300 miles per hour (500 km/h) to around 600 miles per hour (1,000 km/h) in

4482-474: The engine limitation has resulted in the necessity of strict weight control. The CSIST 's Tien Chien (Sky Sword) project was slightly more independent, since it was considered to be a development for all the ROCAF's aircraft rather than only the IDF. The Tien Chien 1 (TC-1) is a short range infrared-seeking missile with an external configuration similar to that of the AIM-9 Sidewinder , while

4565-407: The external fuel lines were detached. However, keeping QRA aircraft at this state of readiness was physically and mentally draining to the pilots and was expensive in terms of fuel. As an alternative, longer-range designs with extended loiter times were considered. These area defense interceptors or area defense fighters were in general larger designs intended to stay on lengthy patrol and protect

4648-480: The government would include a new budget allocation for the IDF upgrade plan (as included in the five MND proposals to help AIDC). The five proposals were: In 2001, it was reported that development of a new " stealth " variant with more powerful engines and improved fire-control system would commence that year. In a 2006 interview with Jane's Defence Weekly , former AIDC Chairman Sun Tao-Yu said that two new prototypes had been manufactured. The upgrade would allow

4731-400: The intended article. Retrieved from " https://en.wikipedia.org/w/index.php?title=Ck1&oldid=1125585096 " Category : Letter–number combination disambiguation pages Hidden categories: Short description is different from Wikidata All article disambiguation pages All disambiguation pages AIDC F-CK-1 Ching-kuo Taiwan initiated the IDF program when

4814-479: The interceptor role until it received upgrades in the 1990s for ground attack. Both the fighter and the Phoenix missile were retired in 2006. The British Royal Air Force operated a supersonic day fighter, the English Electric Lightning , alongside the Gloster Javelin in the subsonic night/all-weather role . Efforts to replace the Javelin with a supersonic design under Operational Requirement F.155 came to naught. The UK operated its own, highly adapted version of

4897-475: The interceptor role. Day interceptors have been used in a defensive role since World War I , and are perhaps best known from major actions like the Battle of Britain , when the Supermarine Spitfire and Hawker Hurricane were part of a successful defensive strategy. However, dramatic improvements in both ground-based and airborne radar gave greater flexibility to existing fighters and few later designs were conceived as dedicated day interceptors. Exceptions include

4980-423: The next generation of light strike and advanced trainer aircraft", with a thrust of 4260 lbf (18.9 kN) dry and 6790 lbf (30.2 kN) with afterburner. After the initial negotiation, the investment was going to be divided between Garrett, Volvo, AIDC, and the Italian company Piaggio . The development would consist of the non-afterburning TFE1042-6 for light attack aircraft and advanced trainers, and

5063-479: The only widely used examples designed after the 1960s being the Panavia Tornado ADV , Mikoyan MiG-25 , Mikoyan MiG-31 , and the Shenyang J-8 . The first interceptor squadrons were formed during World War I to defend London against attacks by Zeppelins and later against fixed-wing long-range bombers . Early units generally used aircraft withdrawn from front-line service, notably the Sopwith Pup . They were told about their target's location before take-off from

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5146-436: The overall mission time, there were few ways to reduce this. During the Cold War in times of heightened tensions, quick reaction alert (QRA) aircraft were kept piloted, fully fueled and armed, with the engines running at idle on the runway ready to take off. The aircraft being kept topped up with fuel via hoses from underground fuel tanks. If a possible intruder was identified, the aircraft would be ready to take off as soon as

5229-459: The project. Joint investment with Garrett became the only practical solution. In 1978, following the success of the TFE731 engine, U.S. engine company Garrett announced joint research of the TFE1042 afterburner with the Swedish company Volvo Flygmotor . The TFE731 Model 1042 was touted as a low bypass ratio "military derivative of the proven commercial TFE731 engine" and that it would provide "efficient, reliable, cost effective propulsion for

5312-515: The radar". By flying terrain masking low-altitude nap-of-the-earth flight profiles the effective range, and therefore reaction time, of ground-based radar was limited to at best the radar horizon . In the case of ground radar systems this can be countered by placing radar systems on mountain tops to extend the radar horizon, or through placing high performance radars in interceptors or in AWACS aircraft used to direct point defense interceptors. As capabilities continued to improve – especially through

5395-411: The reliance on US controlled source code. The first test flight of the upgraded IDF was reportedly successfully completed a few days ahead of schedule in early October. On March 27, 2007, President Chen Shui-Bian witnessed a test flight of F-CK-1D, and announced that the upgraded IDF will be named Hsiung Ying (Brave Hawk), which signifies that the new fighter would protect the homeland just like

5478-445: The removal of the fire control radar and combat systems with the retention of rear-seat flight controls, so that the IDF could be used as a lead-in fighter trainer (LIFT). The ROCAF seemed to have reservations with the concept, however, as it would mean the IDF LIFT would not be usable in wartime. A MND letter said, "Regarding the newspaper report of AIDC's desire to use the IDF fighter as a basis for supersonic trainer development, it

5561-404: The role merged with that of the heavy air superiority fighter . The interceptor mission is, by its nature, a difficult one. Consider the desire to protect a single target from attack by long-range bombers. The bombers have the advantage of being able to select the parameters of the mission – attack vector, speed and altitude. This results in an enormous area from which the attack can originate. In

5644-470: The same time, GD worked on the G configuration in parallel. Eventually the G-4 was selected, but with many features of the C-2 integrated. During this time, the project was named the "Light Weight Defense Fighter". In 1985, the configuration conceptual design had evolved into the SE-1 preliminary design. By the end of 1985, AIDC decided to skip the prototype stage and go into Full Scale Development (FSD) directly, in order to reduce time and save money. The project

5727-450: The second type was exemplified historically by specialized night fighter and all-weather interceptor designs, the integration of mid-air refueling, satellite navigation, on-board radar, and beyond visual range (BVR) missile systems since the 1960s has allowed most frontline fighter designs to fill the roles once reserved for specialized night/all-weather fighters. For daytime operations, conventional light fighters have normally filled

5810-436: The single-engine Bell P-39 Airacobra and the twin-engine Lockheed P-38 Lightning . Both aircraft were successful during World War II in standard fighter roles, not specifically assigned to point defense against bombers. From 1946 to 1980 the United States maintained a dedicated Aerospace Defense Command , consisting primarily of dedicated interceptors. Many post-war designs were of limited performance, including designs like

5893-486: The time it takes for the bombers to cross the distance from first detection to being on their targets, the interceptor must be able to start, take off, climb to altitude, maneuver for attack and then attack the bomber. A dedicated interceptor aircraft sacrifices the capabilities of the air superiority fighter and multirole fighter (i.e., countering enemy fighter aircraft in air combat manoeuvring ), by tuning its performance for either fast climbs or high speeds. The result

5976-660: The upgrade essentially used the TFE1088-11 configuration, to reduce political interference ITEC renamed the original, lower-thrust version as the TFE1042-X70 and retained the TFE1042-70 designation for the upgraded version. In 1988, ITEC decided to invest in the 12,000 lbf (53 kN) thrust TFE1088-12, which was re-designated as the TFE1042-70A for political reason as well. Preliminary studies had shown that

6059-406: The upgraded 32-bit IDF C/D flight control computer was awarded in 2002 to BAE Systems. AIDC said that the improvements of the flight computer will result in "a safer, higher-performing aircraft.” Other improvements made include enhanced electronic warfare capabilities, a strengthened landing gear and a digital anti-skid system. The upgrade also included new indigenous flight control software ending

6142-420: The widespread introduction of the jet engine and the adoption of high speed, low level flight profiles, the time available between detection and interception dropped. Most advanced point defence interceptors combined with long-range radars were struggling to keep the reaction time down enough to be effective. Fixed times, like the time needed for the pilot to climb into the cockpit, became an increasing portion of

6225-472: Was a prototype jet fighter developed during the 1950s. It never flew and was cancelled in 1960. The Canadian subsonic Avro Canada CF-100 Canuck served in numbers through 1950s. Its supersonic replacement, the CF-105 Arrow ("Avro Arrow"), was controversially cancelled in 1959. The Swedish Saab 35 Draken was specifically designed for intercepting aircraft passing Swedish airspace at high altitudes in

6308-549: Was again renamed into the "Indigenous Defense Fighter". Four FSD aircraft were made, with three single-seaters and one double-seater. The IDF is equipped with a GD-53 Golden Dragon multi-mode monopulse pulse-Doppler radar , which is based on the General Electric AN/APG-67 X band radar developed for the F-20 while sharing some components and technologies of the AN/APG-66 radar of the F-16A, and using

6391-805: Was awarded a production contract and options totaling $ 116.2 million by the Aerospace Industrial Development Corporation for Improved Radar Warning Receivers (IRWR) to be installed aboard. Exports of advanced engines such as the General Electric F404 or the Pratt & Whitney F100 were not available to Taiwan and both the General Electric J85 and General Electric J79 were considered unsuitable in their performance, and most European and American engine companies declined to cooperate with

6474-512: Was cut to 130 in 1991, following deals for the purchase of 150 F-16 Block 20 A/B and 60 Mirage 2000-5Ei/Di with the US and France . The 130 included 28 two-seaters and the 10 pre-production units. The first production units were delivered in early 1994, and the program concluded in 2000. The first squadron entered service during the latter part of the 1994. Mid-life updates to the aircraft were initiated in 2011. The Ministry of National Defense (MND) announced that beginning in 2001,

6557-544: Was designated for deployment of interceptors. The aircraft of the Soviet Air Defence Forces (PVO-S) differed from those of the Soviet Air Forces (VVS) in that they were by no means small or crudely simple, but huge and refined with large, sophisticated radars; they could not take off from grass, only concrete runways; they could not be disassembled and shipped back to a maintenance center in

6640-652: Was designed primarily as a stealth air superiority fighter. In the 1950s, the United States Navy led an unsuccessful F6D Missileer project. Later it launched the development of a large F-111B fleet air defense fighter, but this project was cancelled too. Finally, the role was assigned to the F-14 Tomcat , carrying AIM-54 Phoenix missiles. Like the USAF's F-15, the USN's F-14 was also designed primarily as an air superiority (fighter-to-fighter combat) and F-14s served

6723-522: Was for interceptors as the Commonwealth and American air forces pounded German targets night and day. As the bombing effort grew, notably in early 1944, the Luftwaffe introduced a rocket-powered design, the Messerschmitt Me 163 Komet , in the very-short-range interceptor role. The engine allowed about 7 minutes of powered flight, but offered such tremendous performance that they could fly right by

6806-401: Was never completely dispelled. In 1985, the preliminary review of the IDF's design revealed some performance requirement shortfalls, and it was determined that an upgrade of engine thrust by 10% was the simplest solution. Due to American export license restrictions, ITEC used FADEC to artificially limit the thrust below a certain altitude (the restriction was not removed until 1990). Although

6889-552: Was never produced. The first stage of upgrades to the fleet was originally planned to be completed by 2013, and was planned to include improved avionics, radar, electronics, weapons capabilities and lifespan extensions. In May 2014, the ROC Air Force made photos of the fighters with enhanced Wan Chien long-range missile capabilities public. The upgrade program was finally completed in 2018. Four "Full Scale Development" units were produced; three single-seaters followed by

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