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RAF Lossiemouth Military Fast Jet Eurofighter Typhoon FRG4 Registration Serial ZK342. SCO 11,235.

RAF Lossiemouth Military Fast Jet Eurofighter Typhoon FRG4 Registration Serial ZK342.  SCO 11,235. Stock Photo
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Image details

Contributor:

David Gowans / Alamy Stock Photo

Image ID:

GT3493

File size:

70 MB (2.6 MB Compressed download)

Releases:

Model - no | Property - noDo I need a release?

Dimensions:

5914 x 4135 px | 50.1 x 35 cm | 19.7 x 13.8 inches | 300dpi

Date taken:

16 August 2016

Location:

RAF Lossiemouth, Moray. Grampian Region. Scotland. UK.

More information:

The Eurofighter Typhoon is a twin-engine, canard-delta wing, multirole fighter. The Typhoon was designed and is manufactured by a consortium of three companies, Alenia Aermacchi, Airbus Group and BAE Systems, which conduct the majority of affairs dealing with the project through a joint holding company, Eurofighter Jagdflugzeug GmbH, which was formed in 1986. The project is managed by the NATO Eurofighter and Tornado Management Agency, which also acts as the prime customerThe Eurofighter Typhoon is unique in modern combat aircraft in that there are four separate assembly-lines. Each partner company assembles its own national aircraft, but builds the same parts for all aircraft (including exports); Premium AEROTEC (main centre fuselage), EADS CASA (right wing, leading edge slats), BAE Systems (front fuselage (including foreplanes), canopy, dorsal spine, tail fin, inboard flaperons, rear fuselage section) and Alenia Aermacchi (left wing, outboard flaperons, rear fuselage sections).The Typhoon is a highly agile aircraft at both supersonic and low speeds, achieved through having an intentionally relaxed stability design. It has a quadruplex digital fly-by-wire control system providing artificial stability, as manual operation alone could not compensate for the inherent instability. The fly-by-wire system is described as "carefree", and prevents the pilot from exceeding the permitted manoeuvre envelope. Roll control is primarily achieved by use of the wing elevons. Pitch control is by operation of the foreplanes and elevons, the yaw control is by rudder. Control surfaces are moved through two independent hydraulic systems, which also supply various other items, such as the canopy, brakes and undercarriage; powered by a 4, 000 psi engine-driven gearbox. Engines are fed by a chin double intake ramp situated below a splitter plate. Navigation is via both GPS and an inertial navigation system.

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