Flying Over Paradise..

The Mirage 2000 is a French-built multirole fighter jet manufactured by Dassault Aviation.The Mirage 2000 was developed by Dassault-Breguet for the Armée de l'Air as an alternative to the swing-wing Avion de Combat Futur. After the latter was cancelled in 1975 due to its growing cost and complexity, Dassault offered the Mirage 2000 as an alternative. Development of this aircraft would also give the company a competitor to the General Dynamics F-16 Fighting Falcon, which had defeated the Dassault Mirage F1 in a contest for a new fighter for the air forces of Belgium, Denmark, Netherlands and Norway.

The prototype made its first flight in March 10, 1978 with test pilot Jean Coreau at the controls. The first production example flew in November 20, 1982 and the aircraft went into operational service in 1984.Using the concept of the delta wing interceptor seen on the Dassault Mirage III, Dassault built a new design but still using a delta wing. This configuration is not ideal with regard to maneuverability, low-altitude flight, and distance required for take-off and landing, but has advantages in high-speed flight characteristics, simplicity of construction, low radar signature and internal volume.# Low-set thin delta wing with cambered section, 58 degrees leading-edge sweep and moderately blended root; area-ruled; capable of carrying four air-to-air missiles.
# 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 of 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.Multi-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.The aircraft has a redundant fly-by-wire automatic flight control system, providing a high degree of agility and easier handling.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.

The instrument panel 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. * 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. * Thomson-CSF RDM multi-mode radar or Dassault Electronique/Thomson-CSF RDI pulse-Doppler radar for Mirage 2000C/D, each with operating range of 54 nm (100 km / 62 miles). * Dassault/Thales Antilope 5 Radar with terrain avoidance capability for Mirage 2000N Nuclear Strike variant. * The Thales multimode RDY (Radar Doppler Multitarget) developed for Mirage 2000-5.
The Mirage 2000 is equipped with a SNECMA M53-5 or SNECMA M53-P2 turbofan engine according to the different Mirage 2000 versions, 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 3978 liters in Mirage 2000C and E, and 3904 liters in Mirage 2000B, N, D and S. There are also provisions for a jettisonable 1300-liter centerline fuselage fuel tank and for a 1700-litre drop tank under each wing.