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Dassault Rafale

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Dassault Rafale
Dassault Rafale

Dassault Rafale
Description
Role Multi-role fighter aircraft
Crew 1 or 2
First Flight 1986 (demonstrator)
Entered Service 2002
Manufacturer Dassault Aviation
Dimensions
Length 15.30 m 50 ft 2 in
Wingspan 10.90 m 35 ft 9 in
Height 5.34 m 17 ft 6 in
Wing area 46 m² ft²
Weights
Empty 9,060 kg 19,975 lbs.
Loaded 14,710 kg 32,430 lbs.
Maximum takeoff 19,500 kg 42,990 lbs.
Powerplant
Engines 2 × Snecma M88-2
Thrust 50.01 kN (mil.)
75.00 kN (aft.)
11,244 lbs.
16,861 lbs.
Performance
Maximum speed km/h mph
Combat range 1850 km 1150 miles
Ferry range km miles
Service ceiling 16,750 m 55,000 ft
Rate of climb m/min ft/min
Wing loading 320 kg/m² 65.6 lbs/ft²
Thrust/Weight 1.04
Avionics
Avionics Thales RBE2 radar
Thales Spectra aircraft survival system
Thales/SAGEM OSF infrared search and track system
Armament
Guns 30mm DEFA 719B cannon
Bombs Conventional bombs
Missiles 8 AAMs - MICA, AIM-9 Sidewinder, AIM-132 ASRAAM, AIM-120 AMRAAM
air-to-ground weapons inc. MBDA Apache, SCALP EG
ASMP nuclear missile

The Rafale is a French twin-engine delta multirole fighter aircraft designed and built by Dassault Aviation. It is being produced both for land-based use with the French air force and for carrier-based naval operation with the French Navy. The aircraft has undergone a protracted development, for reasons mostly political and economic; the first demonstrator flight was in 1986 but the first production aircraft entered service only in 2002. No foreign sales have yet transpired.

Table of contents
1 History
2 Variants

History

In the early 1980s, both the French Air Force (Armée de l'Air) and Navy (Aéronavale) had a requirement (the Navy's being rather more pressing) to find a new generation of fighter, and their requirements were similar enough to be merged into one project. Collaboration with other European nations was considered, but soon rejected; France produced their own fighter, while the UK, Germany, Italy and Spain collaborated on the similar Eurofighter Typhoon.

Dassault was authorised to work on a technology demonstrator in 1983 named the Rafale ("Squall"). This Rafale A was rolled out in late 1985 and flying in mid 1986. The SNECMA M88 engines being developed were nowhere near ready, so the demonstrator flew with General Electric F404-GE-400 afterburning turbofans as used on the F/A-18 Hornet. The demonstrator impressed the French Ministry of Defence enough to place production orders in 1988. Further testing continued, including carrier touch-and-go landings and test-flying early M88 engines, before the Rafale A was retired in 1994.

Three versions of Rafale were in the initial production order:

The prototype Rafale C flew in 1991, the first of two Rafale M prototypes flew later that year, the prototype Rafale B flew in early 1993 and the second Rafale M prototype flew later that year. Catapult trials were initially carried out at NAS Lakehurst in New Jersey, USA, France having no land-based catapult test facility.

Initially the Rafale B was to be just a trainer, but Gulf War and Kosovo experience showed that a second crewmember is invaluable on strike and reconnaissance missions, and therefore more Rafale Bs were ordered, replacing some Rafale Cs. A similar decision was made by the Navy, who initially did not have a two-seat aircraft on order; this was at first called the Rafale BM but soon became the Rafale N.

Political and economic uncertainty meant that it was not until 1999 that a production Rafale M flew. The marine version has priority since the aircraft it is replacing are much older, especially the Vought F-8 Crusader fighter which is a 50 year old design. Service deliveries began in 2001 and the first squadron became fully operational on the Charles de Gaulle in 2002

Variants

Rafale A

This was a technology demonstrator that first flew in 1986, as described above. It has now been retired.

Rafale D

Dassault used this designation (D for discret or stealthy) in the early 1990s for the production versions for the Armée de l'Air, to emphasize the new semi-stealthy features they had added to the design.

Rafale B

This is the 2-seater version for the Armée de l'Air; to enter service in 2004.

Rafale C

This is the single-seat version for the Armée de l'Air; to enter service in 2004

Rafale M

This is the carrier-borne version for the Aéronavale, which entered service in 2001. Very similar to the Rafale C in appearance, the M differs by:

The Rafale M weighs about 500 kg (1,100 lbs.) more than the Rafale C. Unusually for a carrier-based plane, it does not have folding wings. This was to save money by increasing commonality with the land-based Rafales.

The initial deliveries have been F1 (Fase 1 - Phase 1) aircraft, capable of only air-to-air combat with no air-to-ground capability, to replace the ageing F-8 Crusader in the carrier-based fighter role. Additional deliveries of F2 air-to-ground capable aircraft will replace the Dassault Super Etendard in the attack role and the Dassault Etendard IVP in the reconnaissance role, leaving the Rafale M and Rafale N as the only armed fixed-wing aircraft flown by the Aéronavale. F3 aircraft will have terrain-following 3D radar and nuclear capability.

Rafale N

The Rafale N, originally called the Rafale BM, is a 2-seater version for the Aéronavale. Originally the Aéronavale did not plan to acquire any 2-seaters for combat purposes, but experience in the Gulf and Kosovo taught the usefulness of a second crewmember.

Rafale over EgyptEnlarge

Rafale over Egypt

Rafale flyingEnlarge

Rafale flying

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