Modern Drawings/Air/Arabia Saudi/Others/Typhoon_2Seater.htm | Update: -


 

 

First Typhoon delivery for Oman.

 

Specifications
General

Type: Fighter-Trainer
Crew: 2
First flight: 27 March 1994
Introduction: 4 August 2003
Number built: 2 delivred + 10 ordered (1/2-Seater variants ?)
Powerplant
2 × Eurojet EJ200 afterburning turbofan
Dry thrust: 60 kNeach
Thrust with afterburner: 89 kN each
Dimensions/Masses
Length: 15.96 m | Wingspan: 10.95 m | Height: 5.28 m
Wing area: 51.2 m²
Empty weight: 11150 kg | Max takeoff weight: 23500 kg
Performances
Maximum speed: Mach 2 (2475 km/h)
Combat radius: 1389 km | Ferry range: 2900 km
Service ceiling: 19812 m
Armament

Inside: 1 × 27 mm Mauser BK-27 Revolver gun (150 rounds)
Outside: Total of 13: 8 × under-wing; and 5 × under-fuselage pylon stations; holding up to 7500 kg of payload

 

 

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