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 lb |
| Loaded | 14,710 kg | 32,430 lb |
| Maximum takeoff | 19,500 kg | 42,990 lb |
| Powerplant | ||
| Engines | 2 × Snecma M88-3 (series) | |
| Thrust | n/d kN (mil.) 87.68 kN (aft.) |
19,710 lbf |
| Performance | ||
| Maximum speed | 2125 km/h | 1321 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 lb/ft² |
| Thrust/Weight | 5.96 N/kg | 0.608 lbf/lb |
| Avionics | ||
| Avionics | Thales RBE2 radar Thales Spectra aircraft survival system Thales/SAGEM OSF infrared search and track system | |
| Armament | ||
| Guns | 1 x 30 mm GIAT 30/719B cannon | |
| Bombs | Conventional bombs | |
| Missiles | air-to-air missile (AAMs) - MICA IR/EM, AIM-9 Sidewinder, AIM-132 ASRAAM, AIM-120 AMRAAM, MBDA Meteor, MAGIC 2 air-to-ground weapons inc. MBDA Apache, SCALP EG, AASM, AM 39 Exocet ASMP nuclear missile | |
The Rafale is a French twin-engine delta-wing 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 mostly political and economic rather than technical reasons; the first demonstrator flight was in 1986 but the first production aircraft entered service only in 2002. No foreign sales have yet being made.
The Rafale carries, for the first time in aviation history, an integrated electronic survival system named SPECTRA which features a software-based virtual stealth technology.
The current Rafale variants are marginally capable of supercruise with light weapons loads. A planned engine upgrade, according to some sources [1], will allow the Rafale to supercruise with more realistic loads at around Mach 1.4.
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. This requirement was initially to be met by the Future European Fighter Aircraft (F/EFA) involving Britain, France, Germany, Italy and Spain.
Differences soon emerged in the project, carrier capability was specific to France only and while France wanted an offensive ground-attack aircraft with secondary air-to-air role the other nations had air-to-air as their primary mission. Dassault was authorised to work on a technology demonstrator in 1983 named the Rafale ("Burst"). The final divergence came in 1985, following French demands for far ranging control of the F/EFA project, including all senior roles within the joint company. France announced its intention to leave the project and committed to the national Rafale. Its former partners continued their collaboration on what was to become the Eurofighter Typhoon.
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:
- Rafale C (Chasseur) Single-seat fighter for the Armée de l'Air
- Rafale B (Biplace) Two-seat fighter for the AdA
- Rafale M (Marine) Single-seat carrier fighter for the Aéronavale
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; the program nevertheless was stopped.
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.
Recently, Singapore held a contest to replace its aging aircraft. The F-15 and the Rafale were both great contenders, but the Rafale was defeated in the mock combat situation, costing France a one billion dollar contract.
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; was delivered in June 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 in the following respects:
- Strengthened to withstand the rigors of carrier-based aviation
- Stronger landing gear
- Longer nose gear leg to provide a more nose-up attitude for catapult launches
- Deleted front center pylon (to give space for the longer gear)
- Large stinger-type arresting hook between the engines
- Built-in power operated boarding ladder
- Carrier microwave landing system
- "Telemir" inertial reference platform that can receive updates from the carrier systems.
The Rafale M weighs about 500 kg (1,100 lb) 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.
Rafale N
The Rafale N, originally called the Rafale BM, was planned to be a 2-seater version for the Aéronavale. Budget constraints and the cost of training extra crew members have been cited as the grounds for its cancellation.
Standards
Initial deliveries of the Rafale M were to the F1 ("France 1") standard. This meant that the aircraft was suitable for air-to-air combat, replacing the obsolescent F-8 Crusader as the Aviation Navale's carrier-based fighter, but unsuited for air-to-ground operations. Future deliveries will be to the "F2" standard, giving air-to-ground capability, and replacing the Dassault Super Étendard in the ground attack role and the Dassault Étendard IVP in the reconnaissance role. This will leave the Rafale M as the only fixed-wing aircraft flown by the Aviation Navale, and plans are to upgrade all airframes to the "F3" standard, with terrain-following 3D radar and nuclear capability, from early in the decade following 2010.
The first Rafale C delivered to the Armée de l'Air, in June 2005, was to the "F2" standard, and it is anticipated that upgrades similar to those of the navy will take place in the future. The Rafale replaces the Mirage F1 and the Mirage 2000 in the Armée de l'Air.
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Rafale over Egypt
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Rafale in flight
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Rafale number 9 on the launching deck of the FS Charles de Gaulle carrier (5th of June 2004)
References
- Flight International article,French Fusion. Retrieved 30 August, 2005.
