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SEPECAT Jaguar

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SEPECAT Jaguar
SEPECAT Jaguar

SEPECAT Jaguar
Description
Role Ground attack
Crew 1
First Flight September 8, 1968
Entered Service 1973
Manufacturer SEPECAT
Dimensions
Length 15.52 m ' "
Wingspan 8.64 m 28' 6"
Height 4.92 m ' "
Wing area 21.18 m² ft²
Weights
Empty 7,700 kg 16,970 lbs
Loaded 11,000 kg 24,149 lbs
Maximum takeoff 15,700 kg 34,612 lbs
Powerplant
Engines 2 × Rolls Royce/Turbomeca RT712 Adour turbofans
Thrust 38.10 kN lbs
Performance
Maximum speed 1,690 km/h 1,056 mph
Combat range 852 km 530 miles
Ferry range 4,210 km 2,600 miles
Service ceiling 13,920 m 45,930ft
Rate of climb m/min ft/min
Wing loading kg/m² lb/ft²
Thrust/Weight
Armament
Guns 2 × 30 mm Aden or DEFA cannon
Bombs 4536 kg on 5 hardpoints
Missiles 2 × AIM-9 Sidewinder
Rockets LAU-5003B/A CRV-7 rocket launchers

The SEPECAT Jaguar is an Anglo-French ground attack aircraft in service with the Armée de l'Air, the Royal Air Force and several export customers, notably India. It was the product of the world's first bi-national military aircraft program.

The Jaguar program began in the early 1960s, in response to a British requirement for an advanced supersonic jet trainer, and a French need for a cheap, subsonic dual role trainer and attack aircraft with good short field performance. From these apparently disparate aims would come a single and entirely different aircraft: relatively high-tech, supersonic, and optimised for ground attack in a high-threat environment. It was planned as a replacement for the RAF Hawker Hunter and the Armee de l'Air F-100 Super Sabre.

Cross-channel negotiations led to the formation of SEPECAT (the Société Européenne de Production de l'Avion d'Ecole de Combat et d'Appui Tactique) in 1966 as a joint venture between Bréguet (the design leader) and the British Aircraft Corporation to produce the airframe, and a separate teaming of Rolls-Royce and Turboméca to develop the Adour afterburning turbofan engine.

The first of 8 prototypes flew on September 8 1968. It was an orthodox single-seat, swept-wing, twin-engine design with a maximum take-off weight in the 15 tonne class, a wingspan of 8.7m, and overall length of 16.8 m. Combat radius on internal fuel was 850 km, maximum speed Mach 1.6 (Mach 1.1 at sea level) and hardpoints were fitted for an external weapons load of up to 10 tonnes.

The Armee de l'Air took delivery of the first production Jaguar in 1973: one of an eventual 160 single-seat Jaguar As. For type conversion training, France also took 40 of the two-seat Jaguar B. The RAF accepted delivery of the first of 165 single-seat Jaguar GR.1s (or "Jaguar S") in 1974. These were supplemented by 35 two-seat trainers, the Jaguar T2 (or "Jaguar B" according to the manufacturer's designation). The proposed M variant, a carrier launched version, was cancelled.

Jaguars were also sold on the export with some success, the largest single customer being India, which built around 100 under license. Other Jaguar operators are Ecuador, Nigeria and Oman.

The Jaguar saw combat during the Gulf War, with the Armée de l'Air and RAF and the Kosovo War with the Armée de l'Air.

The aircraft has been updated several times and remains in front-line service with Britain and France. It is to be replaced by the Eurofighter Typhoon and the Rafale.

Table of contents
1 Units Using the Jaguar

Units Using the Jaguar

Royal Air Force

Armée de l'Air

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