The Mirage 2000 is a French-built multirole fighter jet manufactured by Dassault Aviation. Designed in the late seventies as a lightweight fighter for the Armée de l'Air, it evolved into a successful multirole aircraft now in service in 9 countries with more than 600 airplanes built.Design featuresFrench Mirage 2000C fully armed. * Low-set thin delta wing with cambered section, 58 degrees leading-edge sweep (4 at the exit wing border) and moderately blended root; area-ruled; two small canard wings, fixed, placed just behind the air intakes. The flight commands on the wing are: four elevons (+15/-30°), four slats, four airbrakes (2 above and 2 below each wing.) * Parachute brake is on the tail, just above the engine exhaust. * The aircraft's center of lift was moved in front of its center of gravity, giving the fighter a degree of instability that enhances maneuverability. * A runway arresting hook or fairing for a brake parachute can be fitted under the tail. The landing roll was reduced by robust carbon brakes. The backward-retracting, steerable nose gear features dual wheels, while the main gear features single wheels and retracts inward into the wings. * An airbrake is fitted on top and below each wing in an arrangement very similar to that of the Mirage III. A noticeably taller tailfin allows the pilot to retain control at higher angles of attack, assisted by small strakes mounted along each air intake. * First fighter jet with negative static stability.StructureMulti-spar metal wing; elevons have carbon-fiber skins with AG5 light alloy honeycomb cores; carbon-fiber/light alloy honeycomb panel covers avionics bay; most of the tailfin and all of the rudder are skinned with boron/epoxy/carbon; the rudder has a light alloy honeycomb core.he aircraft has a redundant fly-by-wire automatic flight control system, providing a high degree of agility and easier handling, together with stability and precise control in all situations. Fighter's Airframe is naturally unstable, and so it is coupled with FBW commands to obtain the best agility; however, in override mode it is still possible to exceed a 270 deg/sec roll rate and allows the aircraft to reach 11 g (within the 12 g structural limit), instead of nine when engaged. The system is reliable with no known losses due to its failure.The fighter is available as a single-seat or two-seat multi-role fighter. The aircraft has hands-on-throttle-and-stick (HOTAS) control. The pilot sits on a SEMB Mark 10 zero-zero ejection seat, a license-built version of the British Martin-Baker Mark 10. Contrary to the F-16, the pilot sits in a conventional position, without the heavy slope that the F-16 seat has. The cockpit is quite small, and there is no bubble canopy. Despite this, the cockpit visibility is quite good, but less than the F-16, especially at 'six O' clock' (rear) position.The instrument panel(in Mirage 2000 C) is dominated by a Heads Up Display (HUD) with the VMC 180 radar screen located centrally below it. To the lower left is a stores management panel. Above the stores management panel are the navigation instruments and altimeter. The right half of the instrument panel houses the engine and systems displays. Located on the left side of the cockpit, just ahead of the throttle, are controls for the communications equipment, including the Have Quick secure radio.Standard avionics for the Mirage-2000B/C include: * Sagem ULISS 52 inertial navigation system (INS), TRT radio altimeter. * Sextant TMV-980 data display system (VE-130 head-up and VMC-180 head-down) (two head-down in 2000N/D). The combined head-up/head-level display is collimated at infinity, and presents data relating to flight control, navigation, target engagement and weapon firing. Sensor and system management data is presented on two colored lateral displays. * Dassault Electronique Type 2084 central digital computer, Digibus digital databus (2084 XR in 2000D) and Sextant Avionique Type 90 air data computer. * LMT NRAI-7A IFF transponder, IO-300-A marker beacon receiver, TRT ERA 7000 V/UHF com transceiver, TRT ERA 7200 UHF or EAS secure voice communications.EnginesMirage 2000 taking off with full afterburner.The Mirage 2000 is equipped with a SNECMA M53-5 (first 37 airplanes), or SNECMA M53-P2 low-baypass ratio turbofan engine, depending on the aircraft version, which provides 64 kN of thrust dry and 98 kN in afterburner. The air intakes are fitted with an adjustable half-cone-shaped centerbody, which provides an inclined shock of air pressure for highly efficient air intake. Total internal fuel capacity is 3,978 litres in the Mirage 2000C and E, and 3,904 litres in the Mirage 2000B, N, D and S. There are also provisions for a jettisonable 1,300-litre centerline fuselage fuel tank and for a 1,700-litre drop tank under each wing. (more)

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