Fighter Jet Mirage - The Dassault Mirage 2000 is a fourth-generation Frchi multirole single-engine jet fighter manufactured by Dassault Aviation. It was designed in the late 1970s as a light fighter to replace the Mirage III of the French Air Force (Armée de l'air). The Mirage 2000 evolved into a multi-role aircraft with several variants developed and sold to many countries. It later evolved into the Mirage 2000N and 2000D strike variants, the improved Mirage 2000-5 and several export variants. Over 600 aircraft have been produced and are in service in nine countries.
The origins of the Mirage 2000 can be traced back to 1965, when France and Great Britain agreed to develop a rotary-wing "Anglo-French Variable Geometry Aircraft" (AFVG). Two years later, France abandoned the project due to cost, after which Britain would work with West Germany and Italy to produce the Panavia Tornado. Dassault instead focused on its variable-geometry aircraft, the Dassault Mirage G experimental prototype. The design was to be realized in the Mirage G8, which would replace the popular Mirage III in service with the French Air Force.
Fighter Jet Mirage
The Mirage 2000 began as a secondary project named "Delta 1000" in 1972. Dassault focused heavily on the Mirage G8A, a fixed-geometry derivative of the Mirage G8 that was a competitor to the Panavia Tornado. Considered the "Avion de Combat Futur" (ACF or Future Combat Aircraft) of the French Air Force (Armee de l'Air, AdA), the Mirage G8 did not fit the concept of future aircraft service. AdA wanted a Mach 3 fighter, not fighter jets, which the Mirage G8 was. As such, Dassault redesigned the Mirage G8 into the twin-engine Super Mirage G8A, which proved ambitious and exclusive, costing two and a half times the price of the Mirage F1, and was overengineered, especially compared to the F-16. which has just received orders from several Europeans from the country. Subsequently, 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 first and a fighter second, while the Delta 2000 was the opposite, but the single-engine Delta 2000 was much more affordable. At the same National Defense Council meeting, the re-designated Mirage 2000 was offered to the AdA and three prototypes were ordered. AdA issued official requirements in March 1976, with parameters matching performance estimates for new Dassault fighters. The aircraft's primary role was interception with a second ground attack option; AdA had a commitment for 200 aircraft. The first aircraft was to be delivered in 1982.
It was a return to the first generation Mirages, but with a number of significant upgrades that attempted to address their shortcomings.
Production of the Mirage 2000 involved three construction sites, two of which were located in Bordeaux and specialized in different components. The wings were made in Martignas and the fuselages were made in Argteuil (northwest of Paris) with final assembly in Bordeaux-Merignac. However, the first prototype, Mirage 2000 No. 01, was built by hand in St Cloud before being transported to the Dassault plant in Istres for assembly. Under Jean Coureau, Flight 1 made its first flight on March 10, 1978, just 27 months after the program began. During the 65-minute flight, Coureau took the aircraft to Mach 1.02 without afterburner, then climbed to an altitude of more than 12,000 m and accelerated the aircraft to 1.3.
By May d the aircraft had exceeded Mach 2 and an air speed of 1,200 kilometers per hour (650 kn). On the other d of the speed spectrum, the Mirage 2000 proved to be a capable low-speed aircraft, as demonstrated at the Farnborough Air Show in September 1978, during which Dassault pilot Guy Mitaux-Maurourd raised the aircraft's nose to a 25° angle. attack. (AoA) when the aircraft decelerated to 190 km/h (100 kn). Later tests showed that the aircraft could achieve an AoA of 30° while carrying fuel tanks and weapons.
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Another prototype, No. 02, made its 50-minute maiden flight in September 1978 under Maurourd. The aircraft was supposed to test some avionics systems and weapons carriers. Loss of aircraft due to flameout on landing in May 1984. First flight of No. 03 in April 1979; equipped with a complete weapon system, it was used to test radars and weapons. After 400 flight hours, it was the Ctre d'Essais Voli, the flight test center. Although three prototypes were ordered in December 1975, Dassault designed another fourth single-seat demonstrator for its own use, which incorporated lessons learned from earlier aircraft, namely reduced fin height and increased fin movement, redesigned air intakes and FBW. System. The test program's only two-seat Mirage 2000B first flew on 11 October 1980.
Deliveries to AdA began in 1983. The first 37 Mirage 2000Cs delivered were equipped with a Thomson-CSF radar-Doppler multifunction device (RDM) and powered by a SNECMA M53-5 turbocharger. 38. The Mirage 2000C had an improved SNECMA M53-P2 turbofan engine. Radar Doppler à Impulse (RDI) built by Thales for the Mirage 2000C in 1987. It has a much longer range of around 150 km and is coupled with Matra Super 530D missiles which are far superior to the older Super 530F. . Look-down/shoot-down capabilities are also greatly improved, but this radar is not typically used for air-to-ground roles.
The Mirage 2000N is a special nuclear strike variant that was designed to carry Air-Sol Moyne Portée (ASMP) nuclear missiles. Flight tests of the first of two prototypes, the Mirage 2000N 01 (the eighth Mirage 2000), began on February 3, 1983. During a 65-minute flight, the aircraft reached a speed of Mach 1.5.
A special conventional attack variant closely derived from the Mirage 2000N is called the Mirage 2000D. The first flight of the Mirage 2000D prototype, a modified prototype of the Mirage 2000N, took place on 19 February 1991. The first flight of the production aircraft took place on 31 March 1993, and entry into service followed in April 1995. 75 and 86 Mirage 2000N and Mirage 2000D were produced.
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By the late 1980s, the Mirage 2000 was becoming obsolete compared to the latest F-16 fighter models. Attention was paid in particular to the aircraft's inability to measure multiple targets at once and the small load of air-to-air missiles it could carry. As a result, Dassault announced in April 1989 that it would begin work in collaboration with Thomson-CSF on a privately funded upgrade of the Mirage 2000C, to be called the Mirage 2000-5.
The two-seat Mirage 2000B prototype was extensively modified as the first Mirage 2000-5 prototype and first flew on 24 October 1990. The Mirage 2000C prototype was also rebuilt to a similar standard and made its first flight on 27 April 1991. a variant of the aircraft designed specifically for the export market, Taiwan -wan was the first country to order the type in 1992, followed by Qatar in 1994. The type was first delivered in 1996 and entered service in 1997.
Domestically, Dassault needed an order from AdA to help boost foreign sales, and in 1993 AdA decided to upgrade 37 of its existing Mirage 2000s to the 2000-5 specification, a transition period before Rafale service arrived at AdA. The improved aircraft were redesignated the Mirage 2000-5F and entered service in 2000. They retained the old Serval/Sabre/Spirale countermeasures and did not gain the ICMS 2 system. display and no built-in cannon, although the pods can be carried.
At the insistence of the United Arab Emirates, Dassault worked on a further modification of the Mirage 2000-5. Originally named the Mirage 2000-9, the variant had an upgraded radar and associated avionics, a changed weapons configuration, and an extended range.
Taiwanese Air Force Grounds Mirage 2000 Fleet Following Crash
The aircraft uses Messier-Dowty retractable tricycle landing gear with two nose wheels and one wheel on each main landing gear. A runway tail hook or brake parachute cover can be installed under the tail surface, which can work with carbon landing gear brakes for short landing distances. A removable refueling sensor can be attached in front of the cockpit, which is moved slightly to the right of the meter.
The Mirage 2000 is available as a single-seat or two-seat multirole fighter. The pilot controls the aircraft using the ctre knob and the left throttles, both of which have HOTAS controls. Pilot sits on SEM MB Mk10
The instrument panel (Mirage 2000 C) is dominated by a Sextant VE-130 windshield, which stores flight control, navigation, targeting and gunnery data, and below that is a radar screen.
The SNECMA M53 afterburner turbofan was developed for the ACF and was available for the Mirage 2000 project. It is a single shaft
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