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Music
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Edited by en52
Music Used
Ravel - Bolero
HEVIA - El Garrotin
Pink Floyd - Learning To Fly
Pink Floyd - One Of These Days
Metallica - Wasting my Hate
Tyler Bates - Returns a King
Greece participated in NATO "nuclear weapons sharing" until 2001, using A-7 Corsair IIs to deploy tactical B61 nuclear warheads from Araxos Air Base. Greece then strategically decided to remove all nuclear weapons under storage in Greece and did not purchase any more aircraft with nuclear mounting capabilities.
In September 2004 started the Mirage 2000BG/EG fleet upgrade to the standard 2000-5 Mk2 and the project was undertaken by the French manufacturer Dassault and the Hellenic Aerospace Industry (EAB). Fifteen aircraft were ordered, while ten more were undertaken for upgrade by Dassault and EAB. The enhancements include upgraded radar and avionics, air-refueling capabilities, new self-defense system and upgraded engine, while the cockpit has taken some serious reforms.
In 2005, Greece was among the first countries to add the F-16 Block 52+ to its inventory. Ninety of these 4.5th [3] generation aircraft were ordered and delivery begun the same year. This advanced F-16 type is an improved version of the Block 50 featuring a more powerful radar, better communications systems and an upgraded engine. The Hellenic Air Force's Block 52+ belong to the 337, 340 and 343 Squadrons with call signs "Ghost", "Fox" and "Star" respectively. 337 SQ is based at Larissa Air Force Base (110 Combat Wing) and the other two in Souda AB (115 CW).
As of 2008, the Hellenic Air Force has a combat fleet of 358 modern or upgraded aircraft. Due to the retirement of units that have ended their operational life (A-7E Corsair II), the HAF should be looking forward to acquiring new 4th, 4.5th or 5th generation fighters in order to reach a total number of 300 advanced fighters, according to the "2007 Supreme Air Force Council Momentum" which was published in 2007. This goal cannot be reached in the foreseeable future due to the slow down of the performance of the Greek economy for the years 2007-2008.
The Hellenic Air Force (HAF) (Greek: Πολεμική Αεροπορία (ΠΑ), Polemikí Aeroporía) is the air force of Greece. The mission of the Hellenic Air Force is to guard and protect the Greek airspace, provide air assistance and support to the Hellenic Army and the Hellenic Navy as well as humanitarian aid (upon request) in Greece and around the world.
During the period of monarchy (1935-1973) the force was known as the Hellenic Royal Air Force (Ελληνική Βασιλική Αεροπορία (EBA), Ellinikí Vasilikí Aeroporía).
The motto of the Hellenic Air Force is "Αίεν Υψικρατείν" meaning "Always Dominate the Heights" and the HAF ensign represents a flying eagle in front of the Hellenic Air Force roundel. The Hellenic Air Force is one of the three branches of the Hellenic Armed Forces.
Until the late 1980s the Air Force deployed Nike-Hercules Missiles armed with U.S. nuclear warheads. As a result of Greco-Turkish tensions around the 1974 Turkish invasion in Cyprus, the U.S. removed its nuclear weapons from Greek and Turkish alert units to storage. Greece saw this as another pro-Turkish move by NATO and withdrew its forces from NATO's military command structure from 1974 to 1980.
In 1988 the first fourth[2] generation fighters were introduced, marking the beginning of a new era: the first Mirage 2000 EG/BG aircraft were delivered to the 114 Combat Wing and equipped the 331 and 332 squadrons. In January 1989, the first F-16C/D Block 30 arrived in Nea Anchialos (111 Combat Wing) and were allocated between the 330 and 346 squadrons.
In March 29, 1991 the RF-84F were retired from service after 34 years and 7 months of operational life. In November 1992 more RF-4E were delivered to the 348 Tactical Reconnaissance Squadron.
In 1997 the reception of fourth generation aircraft continued. In July, delivery of forty F-16 Block 50 began. The new aircraft, equipped with the LANTIRN navigation and targeting pod as well as AMRAAM and HARM missiles, were allocated to the 341 and 347 squadrons.
haf hellas hellenic greece greek air force aegean macedonia thrace tuaf turkey iaf israel dogfight flight cockpit f-102 f102 f 102 mirage 2000 2000-5 mk2 a7 a-7 a-7e a-7h corsair vought f-4 f4e rf-4 phantom fantom spook f-16 f16 falcon viper block 30 40 52 52+ advanced t-2 t2e t-2e buckeye t-6 t6 texan f-5 freedom fighter dassault f1 f-1 keat sot ikarwn ikaron pea 120 sholi t-37 tweet t37 spin icarus hud avtr low level flight napalm bombing f-86 f-83 noratlas cyprus mission hellenic flame acro team
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The Antonov An-12 (NATO report
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The Antonov An-12 (NATO reporting name: Cub) is a four-engined turboprop transport aircraft. It is the military version of the Antonov An-10.Currently the An-12 is very popular with cargo operators, especially those in the CIS, Africa and the Indian subcontinent.General characteristics
Crew: 5: 2 pilots, flight engineer, navigator, radio operator
Capacity: 90 troops
Payload: 20,000 kg (44,000 lb)
Length: 33.10 m (108 ft 7 in)
Wingspan: 38.00 m (124 ft 8 in)
Height: 10.53 m (34 ft 7 in)
Wing area: 121.7 m² (1,310 ft²)
Empty weight: 28,000 kg (62,000 lb)
Max takeoff weight: 61,000 kg (130,000 lb)
Powerplant: 4× Progress AI-20L or AI-20M turboprops, 4,000 ehp (3,000 kW) each
Performance
Maximum speed: 777 km/h (419 knots, 482 mph)
Cruise speed: 670 km/h (361 knots, 415 mph)
Range:
With maximum fuel: 5,700 km (3,075 nm, 3,540 mi)
With maximum load: 3,600 km (1,945 nm, 2,235 mi)
Service ceiling 10,200 m (33,500 ft)
Rate of climb: m/s (ft/min)
Armament
Guns: 2× 23 mm (0.906 in) cannon Nudelman-Rikhter NR-23 in a tail turret (some aircraft)
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###All Footage Is Taken
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song: Preliator - Globus
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 Mirages built.
The Avion de Combat Futur (ACF) was developed for the French Air Force in the early 1970s. After the ACF was canceled on 18 December 1975 due to its growing cost and complexity, Dassault offered the Mirage 2000 as an alternative. This was a return to the first generation Mirages, but with several important innovations that tried to solve their shortcomings. Project chiefs were B.C. Valliéres, J.Cabrière, J.C. Veber and B.Revellin-Falcoz.
Development of this small 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. Small single-engined fighters were clearly the most appreciated by foreign customers, as experience with the larger, twin-engined Mirage 4000 would show.
The prototype made its first flight in March 10, 1978 with test pilot Jean Coreau at the controls. Despite the new technologies applied, basing the new aircraft on the Mirage III allowed the development of a flyable prototype in only 27 months from the program start to the first flight, even if active service status needed another six years.
In that summer, at the Farnbourgh airshow, this machine displayed not only excellent handling capabilities, but also a full control at 204 km/h and 26 AoA. This was totally unexpected by a delta-wing fighter, and proof how CCD controls were capable of overcoming the delta wing shortcomings related to poor low-speed control, while retaining the advantages, such as low-drag, low RCS, ideal high speed aerodynamics and simplicity, provided by the absence of horizontal tail surfaces. The Mirage 2000 was one of the stars of that airshow and became the direct adversary for the F-16, which shared the CCD control and relaxed stability. 02 Prototype followed in 18 September 1978 and 03 in 26 September 1979. After 400 hours of flight, they were sent to CEV (Centre Experimental du Vol). 04 Prototype was a demonstrator made by Dassault for its own purposes, and finally the first dual-seat M.2000B flew in 11 October 1980.
The first production example flew in November 20, 1982 and the aircraft went into operational service in 1984. They were practically pre-production aircraft, because they had no SARH missiles (RDM-1 radar) and the first model of SNECMA 'Super Atar'. M-53-2. The last Mirage 2000 was delivered on November 23, 2007.The Mirage 2000 is scheduled to be replaced in French service by the Dassault Rafale, which became operational with the French Air Force on June 27, 2006. The Mirage 2000 production line was shut down in November 2007 after the last aircraft had been delivered to the Hellenic Air Force.
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.
The fighter is available as a single-seat or two-seat multi-role fighter. The cockpit incorporates hands-on-throttle-and-stick (HOTAS) control and the pilot sits on a SEMB Mark 10 zero-zero ejection seat (a license-built version of the British Martin-Baker Mark 10). Unlike in the F-16, the pilot sits in a conventional position, without the steep backward slope of the F-16 seat. 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' (rearwards-looking) position.
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HAF F-16 BL 50 341 squadron, 111 CW
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HAF 347S QN (111 CW) op
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HAF 347S QN (111 CW) operates F-16C/D BLK50D LANTIRN. It's code name derives from the Greek mythical hero PerseusF-16C/D Block 30, 50 FIGHTING FALCON
Description
It is a single-seat, single-engine, multiple role fighter, designed for all weather operations and capable of carrying a great variety of weapon systems. Greece has in its air arsenal about 70 F-16s, BLOCK 30 and BLOCK 50. In 1989 Greece purchased 40 BLOCK 30 under the Arms Programme "Peace Xenia I" and in 1997 40 additional BLOCK 50 300 spartans hunting turks over aegean aircraft were delivered to Greece as part of "Peace Xenia II". The Hellenic F-16s BLOCK 30 and BLOCK 50 are based in the air base of Larissa (110 Combat Wing, 346 Squadron "Iason") and in the air base of New Anchialos (111 Combat Wing, 330 "Thunder", 341 "Arrow" and 347 "Perseas" Squadrons). All the Hellenic F-16s wear the "Aegean Ghost" camouflage, which is very efficient in Aegean operational environment.
Specifications: * Crew: 1 (C model), 2 (D model) * Engine: General Electric F110-GE 100 afterburning turbofan (Block 30, 29,000 lbs thrust), General Electric F110-GE 129 (Block 50, 31,000 lbs thrust) * Wing Span: 9.45 m * Length: 14.52 m * Maximum Speed: 2,173 km/h * Service Ceiling: 15,240m or 49,000 ft...
hellas hellenic greek greece airspace aviation
The Lockheed Martin F-16 Fighting Falcon is an American multirole jet fighter aircraft originally developed by General Dynamics for the United States Air Force. Designed as a lightweight fighter, it evolved into a successful multirole aircraft. The Falcon's versatility is a paramount reason it was a success on the export market, serving 24 countries. The F-16 is the largest Western fighter program with over 4,000 aircraft built since production started in 1976. Though no longer produced for the US Air Force, it is still produced for export. In 1993, General Dynamics sold its aircraft manufacturing business to the Lockheed Corporation, which in turn became part of Lockheed Martin after a 1995 merger with Martin Marietta.
The Fighting Falcon is a dogfighter with innovations including a frameless, bubble canopy for better visibility, side-mounted control stick to ease control while under high g-forces, and reclined seat to reduce the effect of g-forces on the pilot. It was also the first fighter aircraft deliberately built to sustain 9-g turns. It has a thrust-to-weight ratio greater than one, providing enough power to climb and accelerate vertically - if necessary.Although the F-16's official name is "Fighting Falcon", it is known to some of its pilots as the "Viper", after the Battlestar Galactica starfighter.
To counter this tendency to depart from controlled flight, the F-16 uses a fly-by-wire flight control system (FLCS), with no mechanical linkages between the stick and rudder pedals and the aerodynamic control surfaces. The flight control computer (FLCC), which is the key component of the FLCS, takes thousands of measurements per second of the aircraft's attitude, and makes corrections to counter deviations from the flight path that were not input by the pilot, allowing for stable flight. This led to a common refrain heard from pilots: "You don't fly an F-16; it flies you".
The FLCC also accepts the pilot's input from the stick and rudder controls, and manipulates the control surfaces in such a way as to produce the desired result without inducing a loss of control (known as "departing" controlled flight). The FLCC incorporates a series of limiters that govern movement in the three main axes (pitch, roll and yaw) based on the jet's current attitude, airspeed and angle of attack, and prevent movement of the control surfaces that would induce an instability such as a slip or skid, or a high angle of attack inducing a stall. The limiters also act to prevent maneuvering that would place more than 9 gs of force on the pilot or airframe.
song Hans Zimmer ( remixed by dj Tiesto ) - He is a pirate
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####Reuploaded####
DOWNLOAD LINK http://www.patricksaviation.com/in/6426?i=INx
The Mirag
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The Mirage 2000 is a French-built multirole fighter jet manufactured by Dassault Aviation.
Development and history
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.
Characteristics
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.
Design features
French Mirage 2000C fully armed.
French Mirage 2000C fully armed. * 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.
Structure
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.
Dassault Mirage 2000C at Paris Air Show 2007
Dassault Mirage 2000C at Paris Air Show 2007
and easier handling.
Landing gear
The aircraft uses a retractable tricycle type landing gear by Messier-Bugatti, with twin nosewheels and a single wheel on each main gear. Hydraulic retraction, nosewheels rearward, main units inward. Oleo-pneumatic shock absorbers. Electrohydraulic nosewheel steering (+/-45 degrees). Manual disconnect permits nosewheel unit to caster through 360 degrees for ground towing].
Cockpit
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.
Avionics
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.
Radar * 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.
Countermeasures * Thales Serval Radar warning receiver (RWR) with antennas on the wingtips and on the rear of the top of the tailfin. * Dassault Sabre RF jammer in a pod below the bottom of the tailfin, with an antenna in a fairing on the front of the tailfin. * Dassault Eclair dispenser system under the tail. This was eventually replaced by a pair of Matra Spirale dispensers, one fitted on an extension behind the rear of each wingroot, giving a total capacity of 224 cartridges.
Engines
Mirage 2000 taking off with full afterburner.
Mirage 2000 taking off with full afterburner.
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.
Armament and payload
The Mirage 2000 can carry up to 6.3 tons (13,900 lb) of stores on nine pylons, with two pylons on each wing and five under the fuselage. A fixed removable refuelling probe can be attached in front of the cockpit, offset slightly to the right of center.
Primary armament of the Mirage 2000 includes: * Matra Super 530 medium-range semi-active radar-guided air-to-air missile on the inboard wing pylons. * Matra Magic short-range infrared-seeking AAM on the outboard wing pylons. * The Mirage 2000C can carry air-to-ground stores such as the Matra 68 mm rocket pods, iron bombs, and cluster bombs.
Built-in armament consisted of twin DEFA 554 (now GIAT 30-550 F4) 30 mm revolver-type cannons with 125 rounds each. The cannons have selectable fire rates of 1,200 or 1,800 rounds per minute.
Variants
Mirage 2000C
French Mirage 2000C
French Mirage 2000C
The first Mirage 2000 to go into service was the single-seat Mirage 2000C interceptor. There were four single-seat prototypes, including the initial Mirage 2000 prototype. The first production Mirage 2000C flew in November 1982. Deliveries began in 1983. The first operational squadron was formed in 1984, the 50th anniversary of the French Air Force. A total of 124 Mirage-2000Cs were obtained by the AdA.
The first 37 Mirage 2000Cs delivered were fitted with the Thomson-CSF RDM (Radar Doppler Multifunction) and were powered by the SNECMA M53-5 turbofan engine. The 38th Mirage 2000C had an upgraded SNECMA M53-5 P2 turbofan engine. The Radar Doppler Impulse (RDI) built by Thales did not enter service until 1987.
Latest upgrades include: * Non-Cooperative Target Recognition (NTCR) mode in RDI Radar allows identification of airborne targets not responding on IFF. * Integration with the new Matra MICA (Missile d'Interception, de Combat et d'Autodefense) IR heat-seeking missile. The radar-guided version of the MICA will not be able to support earlier versions of the Mirage 2000.
Mirage 2000B
Mirage 2000B nose close up.
Mirage 2000B nose close up.
The Mirage 2000B is two-seat operational conversion trainer variant which performed its initial flight on October 11, 1980. The AdA acquired 30 Mirage 2000Bs, with all three of the AdA fighter wings obtaining a few each for conversion training.
Mirage 2000N and 2000D Main article: Dassault Mirage 2000N/2000D
The Mirage 2000N is the nuclear strike variant which was intended to carry the Aerospatiale Air-Sol Moyenne Portee (ASMP) nuclear stand-off missile. Initial flight tests of two prototypes began on February 3, 1983, and the Mirage 2000N entered operational service in 1988. A total of 75 were built.
The Mirage 2000D is a dedicated conventional attack variant developed from the Mirage 2000N. Initial flight of the Mirage 2000D prototype, a modified Mirage 2000N prototype, was on February 19, 1991. The first flight of a production aircraft occurred March 31, 1993, and service introduction followed in April 1995. A total of 86 were built.
Mirage 2000-5
By the late 1980s, the Mirage 2000 was beginning to age compared with the latest models of U.S. F-16 fighters, so Thomson-CSF began work on a privately funded update of the Mirage 2000C which was to be named the Mirage 2000-5. A two-seat Mirage 2000B prototype was extensively modified as the first Mirage 2000-5 prototype, and it first flew on October 24, 1990. A Mirage 2000C prototype was then reworked to a similar standard, making its initial flight on April 27, 1991.
Features: * The Thales multimode RDY (Radar Doppler Multitarget). The RDY radar is the heart of the upgrade, providing true multitarget tracking. It can simultaneously detect up to 24 targets and track the eight highest-priority threats while guiding four MICA EMs to different targets simultaneously. * The updated ICMS 2 countermeasures suite and the Samir DDM missile warning system. ICMS 2 incorporates a receiver and associated signal processing system in the nose for detection of hostile missile command data links. The aircraft's self-protection equipment can be interfaced to a new programmable mission-planning and post-mission analysis ground system. * A new glass cockpit layout borrowed from the Rafale program with three-color MFDs, a dual-linked wide-angle HUD / head-level display, and HOTAS controls. The cockpit is NVG-compatible. * Targeting systems included the Thales TV/CT CLDP laser designation pod which provides the capability to fire laser-guided weapons by day and night. * A two-seater version was developed as well. The back-seater has the HUD but not the associated head-level display, and as with first-generation two-seaters, there are no built-in cannon (although cannon pods can be carried). * The Mirage 2000-5 can also carry the oversized drop tanks developed for the Mirage 2000N, greatly extending its range.
In 1993, the AdA decided to upgrade 37 of their existing Mirage 2000s to the 2000-5 specification as a stopgap before the arrival of the Rafale in AdA service. The upgraded aircraft were redesignated Mirage 2000-5F, and became operational in 2000. They retained the old countermeasures system with the Serval/Sabre/Spirale units and did not receive the ICMS 2 system.
The AdA is now considering upgrades for the type, including the MIDS datalink, MICA IR support, and the Thales Topsight helmet-mounted display / sighting system.
Mirage 2000-5 Mark 2
Dassault extended the improvements of the Mirage 2000-5 a bit further with the Mirage 2000-5 Mark 2, which is an enhanced, fully multirole version of the Mirage 2000-5. It is currently the most advanced version of the Mirage 2000.
Features: * Thales RDY-2 radar. The RDY-2 radar is similar in configuration to the original RDY, but features two new air-to-ground modes, including a high-resolution synthetic aperture radar (SAR) imaging mode with a moving target indicator (MTI) capability to provide an all-weather, day/night targeting capability. The radar features low-probability-of-intercept (LPI) operation, with the output pattern varying in a seemingly random pattern that prevents an adversary RWR from recognizing that it has been targeted. * The high-power Modular Data Processing Unit (MDPU) designed for the Rafale. * A new Thales Totem 3000 INS with ring-laser gyros and GPS capability, providing much greater accuracy, higher reliability, and shorter alignment time replaces the older ULISS 52 system. It works in conjunction with a terrain-following system. * An improved, classified ICMS 3 digital countermeasures suite. * An on-board oxygen generation system (OBOGS). * The cockpit was updated as well, retaining the same general layout but with larger color displays and other modernizations. The Thales Topsight helmet-mounted display / sighting system is offered as an option. * The Mirage 2000-5 Mark 2 includes a datalink for the targeting of MICA ER missiles and can carry the Damocles targeting pod. * Future Upgrades: Thales AIDA visual identification pod; technology used in the Rafale will be also integrated into the Mirage 2000, including infrared and optical sensors for IFF and targeting. It will be used by AdA Mirage 2000-5Fs. Further development of the second-generation type is expected to include a GPS receiver, MIDS datalink, and unspecified long-range sensors.
Topsight E helmet-mounted sight
Topsight E displays critical information, protects the pilot, and provides communications. In the display of critical information, Topsight E has three main functions: * Visual target designation by transmitting the target's line of sight to the nav/attack system. Used with modern missiles, Topsight allows pilots to perform wide off-boresight target designation. * Visual target acquisition using reverse cueing mode where the display symbology guides the pilot's eyes to the target tracked by the aircraft sensors. The nav/attack system provides spatial data. * Situational awareness based on concise display of vital information (tactical, navigation, safety, etc.).
Topsight E has four integrated operational modes: * Navigation is based on ring laser gyro INS with embedded GPS receiver. * Air-to-air weapon delivery includes guns, rockets and high- and low-drag bombs, using continuous computation of impact point (CCIP) and continuous computation of release point (CCRP). * Training includes failure simulations, as well as target and threat simulations. * The Topflight avionics suite features a full glass cockpit and HOTAS control, plus a range of avionics, linked to a 1553 multiplex bus.
Mirage 2000E
"Mirage 2000E" was a blanket designation for a series of export variants of the Mirage 2000. These aircraft were fitted the M53-P2 engine and an enhanced "RDM+" radar, and all can carry the day-only ATLIS II laser targeting pod.
Mirage 2000M (Egypt)
Egypt was the first foreign buyer, ordering 16 single-seat Mirage 2000M and four Mirage 2000BM trainers in late 1981, with deliveries beginning in 1986. The Egyptians also purchased ATLIS II pods and a wide range of appropriate munitions, including Magic and Super 530 AAMs, AS-30L laser-guided ASMs, and Armat anti-radiation missiles.
Mirage 2000H (India)
Indian Air Force Mirage 2000H.
Indian Air Force Mirage 2000H.
India is a major user of the Mirage 2000, having acquired a total of 49 examples, including 42 single-seaters and 7 Mirage two-seaters. The IAF named the Mirage Vajra (Thunderbolt). India also purchased appropriate stores along with the fighters, including ATLIS II pods and laser-guided weapons. * Since India wanted the fighter quickly, the first part of an initial batch of 26 single-seaters and 4 two-seaters was shipped to the Indian Air Force (IAF) beginning in 1985 with the older M53-5 engines. These aircraft were given the designations of Mirage 2000H5 and Mirage 2000TH5. * The second part of this initial batch consisted of 10 more single-seaters with the M53-P2 engine, with these aircraft designated Mirage 2000H. All the first batch was reengined with the M53-P2, with the single-seaters re-designated "Mirage 2000H" and the two-seaters re-designated Mirage 2000TH. * A second batch of six Mirage 2000H single-seaters and three Mirage 2000TH two-seaters was shipped in 1987-1988.
Recent orders: * In 2004, the Indian government approved purchase of ten more Mirage 2000Hs, with these machines featuring improved avionics, particularly an upgraded RDM-7 radar. * The Mirage 2000-5 was the front-runner for a planned Indian Air Force 124+ fighter procurement in which it was competing with the Mikoyan MiG-35, F-16 Falcon and JAS 39 Gripen. However, Dassault announced that Mirage 2000 will be replaced by the Rafale as the contender for the deal since the Mirage 2000 production line is to be closed. * India has announced a $1.9 billion program to arm 52 of its Mirage 2000 aircraft with the MBDA ASRAAM dogfighting missile beginning in 2007. Installation will require new radar, electronic warfare equipment, and updates to the cockpit and data bus. Pilot helmets will require addition of a helmet-mounted sight. These will be the first Mirage aircraft to carry the British missile and Dassault, Thales, and MBDA are to participate in the effort
Mirage 2000P (Peru)
Peru placed an order for 10 single-seat Mirage 2000Ps and 2 Mirage 2000DP trainers. The Peruvians ordered a set of munitions similar to that ordered by Egypt, along with ATLIS II targeting pods.
Mirage 2000-5EI (Taiwan)
ASTAC pod
ASTAC |
