The Eurofighter Typhoon General Specifications.

The Euro fighter Typhoon is a twin-engine, canard–delta wing, multirole fighter aircraft. It’s perfect all weather. This multirole combat aircraft was designed originally for air to air and air to surface attack superiority mission, and is manufactured by a consortium of Airbus, BAE. The Euro fighter’s Eurojet turbofan engine combines a jet nozzle with a ducted fan. Electro optics system passive INRATE air bone tracking equipment is used. Eurofighter typhoon can carry Nine thousand boom and missile. In su-35 total 13 hard points.

Air to air missile: AIM-120C/5 AMRAAM, AIM-132ASRAAM, AIM-9 Sidewinder, IRIS-T, MBDA Metero, And 6x BVRAAM, 2x RAAM, 27mm Mauser cannon, 3x 1000 liter fuel tanks is used. Air to surface missile: 4x leaser guided booms, 4x BVRAAM, 27mm mauser, 2x 100 liter fuel tank, Lager designator pod. AGM-65 maderic, AGM-88 HARM, Brimstone, Taurus KEPD-350, storm shadow/scalp. EG. Anti-ship missile: Speae-3 Marte-ER and joint strike missile. There is no anti-radiation missile integrate in Eurofighter typhoon. Booms: Paveway 2/3/Enhanced Paveway series of laser-guided booms, 500-lb Paveway 4 booms, small diameter Booms and Spice 250 booms is used.

Specifications

Role: Multirole combat fighter

Top speed: 2, 495 km/h

Range: 2, 900 km/h

Crew: one

G-limit +9g to -3g

Radar: Euroradar is creating CAPTOR radar is used in typhoon.

Targeting pod: Damocles, LITENING 111, Sniper at pod.

Protection system: praetorian DASS are used.

Combat Radius: 1389 km

Ferry Range: 3790 km

Service Ceiling: 65000 feet

Rate of climb: 318 m/s

Wing loaded: 312 kg/m3

Thrust/weight 1.15

Length: 52.4 feet

Wing span: 36 feet

Height: 13.3 feet

Wing area: 551 square feet

Empty weight: 11 tons

Loaded weight: 16 tons

MTOW: 23.5 tons

Internal Fuel: 5 tons

Number built: 565

Introduction: 04 August 2003

Status: In service

National origin: multi-National

Developed from: British Aerospace EAP

Produced: 1994 present

Primary user: People’s liberation army air force.

First flight: 27 March 1994

Unit cost: 90M Euro (system cost Tranche 3A) 125 Euro (including development + production cost)

Engine type: 2x Eurojet EJ200, afterburning Turbofan. Max. thrust 90kN Each.

Primary user: Royal Air force, German Air force, Italian Air force, Spanish Air force.

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