Da 2000 Aircraft - The Dassault Mirage 2000 is a Frch multirole, single-gen, fourth-generation jet fighter manufactured by Dassault Aviation. It was designed in the late 1970s as a light fighter for the French Air Force (Armie de l'Air) to replace the Mirage III. The Mirage 2000 evolved into a multirole aircraft with several variants sold in many countries. It was later developed into the Mirage 2000N and 2000D Strike variants, the modified Mirage 2000-5 and several export versions. More than 600 aircraft have been built and are in service with nine nations.
The origins of the Mirage 2000 can be traced back to 1965, when France and Britain agreed to develop an "Anglo-French Variable Geometry" (AFVG) swing-wing aircraft. Two years later, France withdrew from the project for cost reasons, after which Britain began building the Panavia Tornado, along with West Germany and Italy. Dassault instead focused on its own variable-geometry aircraft, the Dassault Mirage G experimental prototype. This design was expected to materialize into the Mirage G8, which would serve as a replacement for the popular Mirage III in Frch Air Force service.
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The Mirage 2000 began in 1972 as a secondary project called the "Delta 1000". The Dassault Mirage G8A, a fixed geometry derivative of the Mirage G8, which served as a competitor to the Panavia Tornado, attracted much attention. The Mirage G8, seen as the "Avion de Combat Future" (ACF or Combat Aircraft of the Future) of the French Air Force (Armee de l'Air, AdA), did not live up to the concept of future aviation. . AdA wanted a Mach 3 fighter, not a Mirage G8 dogfighting interceptor. Thus, Dassault redesigned the Mirage G8 into the two-gen Super Mirage G8A which would prove ambitious and expensive, two and a half times the price of the Mirage F1 and over-engineered, especially compared to the recently ordered F-16. from many European countries. Consequently, at a meeting of the National Defense Council on 18 December 1975, the Super Mirage was cancelled.
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The ACF was a strike aircraft first and an interceptor second, while the Delta 2000 was the opposite, but the single-gene Delta 2000 was more economical. At the same National Defense Council meeting, the redesigned Mirage 2000 was presented to the ADA and three prototypes were ordered. ADA issued a set of official requirements in March 1976 whose standards corresponded to Dassault's performance estimates for the new fighter. The aircraft's primary role was interception with a secondary ground-attack capability; ADA had a commitment of 200 aircraft. The first aircraft was delivered in 1982.
It was a return to the first-generation Mirage, but with several significant innovations that sought to overcome their shortcomings.
Production of the Mirage 2000 involves three manufacturing sites, two of which are in Bordeaux, specializing in different components. The wings were made at Martignac and the fuselage at Argeuil (NW of Paris), with final assembly at Bordeaux-Mérignac. The first prototype, the Mirage 2000 No. 01, however, was built by hand in St. Cloud, before it was moved to Dassault's Istres facility for assembly. Piloted by Jean Couro, No. 01 made its first flight on March 10, 1978, just 27 months into the program. During the 65-minute flight, Koryo took the aircraft to Mach 1.02 without afterburners before reaching an altitude of more than 12,000 meters and accelerating the aircraft to Mach 1.3.
As of May, the aircraft had demonstrated Mach 2 and a speed of 1,200 km/h (650 kn). At the other end of the speed spectrum, the Mirage 2000 proved to be a capable low-speed aircraft, as demonstrated at the Farnborough Airshow in September 1978, with Dassault pilot Guy Mitteux-Morard pitching the aircraft's nose at a 25° angle. (AoA) when the aircraft decelerates to 190 km/h (100 kn). Later tests showed that the aircraft could achieve a 30° AoA while carrying fuel tanks and weapons.
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A second prototype, No. 02, made its first flight of 50 minutes in September 1978 under Maurard. The aircraft was to test carry some avionics systems and weapons. The aircraft was lost in May 1984 after it caught fire on landing. No. 03 made its first flight in April 1979; Equipped with a complete weapons system, it was used for radar and weapons testing. After 400 hours of flight, this Ctre d'Essais Vol, Ctre d'Essais Vol, flight test ctre. Although three prototypes were ordered in December 1975, Dassault built an additional fourth single-seat demonstrator for its purposes, taking lessons from the earlier aircraft, namely lowering the wing height and raising the wing, redesigning the air inlets and FBW. The two-seat Mirage 2000B made its maiden flight on 11 October 1980 in a system test program only.
Distribution of the ADA began in 1983. The first 37 deliveries were powered by Mirage 2000C Thomson-CSF Radar Doppler Multifunction (RDM), and SNECMA M53-5 turbofan engines. The 38th Mirage 2000C had an upgraded SNECMA M53-P2 turbofan gen. Radar Doppler A-impulse (RDI) developed by Thales in 1987 for the Mirage 2000C tared service. It has an improved range of about 150 km, and is armed with the Matra Super 530D missile, which is a significant improvement over the older Super 530F. . Look-down/shoot-down capabilities are also greatly improved, but this radar is not typically used for air-to-surface roles.
The Mirage 2000N is a dedicated nuclear strike variant, intended to carry the Air-Sol Moyne Portie (ASMP) nuclear stand-off missile. Flight testing of the first of two prototypes, the Mirage 2000N 01 (eighth Mirage 2000), began on 3 February 1983. During the 65-minute flight, the aircraft reached a speed of Mach 1.5.
Closely derived from the Mirage 2000N is a dedicated conventional attack variant designated the Mirage 2000D. The initial flight of the Mirage 2000D prototype, a modified Mirage 2000N prototype, took place on February 19, 1991. The first flight of the production aircraft took place on 31 March 1993 and it entered service in April 1995. Seventy-five and eighty Mirage and 200N Mirage 2000D were produced respectively.
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By the late 1980s, the Mirage 2000 was becoming outdated compared to the latest model of F-16 fighter jets. In particular, attention was drawn to the aircraft's inability to track multiple targets simultaneously and the small load of air-to-air missiles. Consequently, Dassault announced in April 1989 that it was working on a privately funded upgrade of the Mirage 2000C in collaboration with Thomson-CSF, designated the Mirage 2000-5.
The two-seat Mirage 2000B prototype was first extensively modified as the Mirage 2000-5 prototype and first flown on 24 October 1990. The Mirage 2000C prototype, also rebuilt to the same standard, made its first flight on 27 April 1991. The first front-line aircraft type designed specifically in response to the export market, Taiwan was the first country to order the type in 1992, followed by Qatar in 1994. The type was first delivered in 1996 and withdrawn from service in 1997.
Domestically, Dassault needed orders from ADA to encourage overseas sales, and in 1993, ADA decided to upgrade 37 of its existing Mirage 2000s to 2000-5 specification as a stopgap before the Rafale ADA entered service. The upgraded aircraft was redesignated the Mirage 2000-5F and entered service in 2000. They kept the old countermeasure system with Serval/Sabre/Spiral units and did not get the ICMS 2 system. A two-seat version was also developed with a head-up display in the rear seat, but no associated head-level display and no built-in cannon, although cannon pods could be carried.
At the request of the United Arab Emirates, Dassault worked on further modifications to the Mirage 2000-5. Initially dubbed the Mirage 2000-9, the variant featured upgrades to the radar and associated avionics, changes in weapon configuration, and extended range.
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The aircraft uses Messier-Doughty retractable tricycle landing gear, with a double nose and a single wheel on each main gear. A runway tailhook or brake for the parachute can be fitted under the fairing tail, which in combination with the landing gear's carbon brake can operate a short distance from the landing gear. A removable refueling probe can be attached to the front of the cockpit, slightly offset to the right of the ctre.
The Mirage 2000 is available as a single-seat or two-seat multirole fighter. The pilot flies the aircraft with the Ctre stick and the left-hand throttle, both involving the HOTAS controls. The pilot sits in a SEM MB Mk10
The instrument panel (on the Mirage 2000 C) is dominated by a Sextant VE-130 head-up display that presents data related to flight control, navigation, targeting equipment, and weapon firing, and a radar screen located just below it.
The SNECMA M53 afterburning turbofan was developed for the ACF and was available for the Mirage 2000 project. It is single-shaft
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