SEPECAT Jaguar

· Bréguet Aviation

Airplanes

Length

16.83 m

Flat Wing Span

8.69 m

Height

4.89 m

Flat Wing Area

24.18 m²

Flat Wing Aspect Ratio

3.12

Max Speed

1350 km/h

Max Ceiling

14000 m

Number of Engines

First Flight

1968-09-08

Entry Into service

1973-01-01

Number Built

573

Maximum Take-Off Weight

15.7 t (paragliders: kg)

Total Fuel Capacity

4200

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity
SEPECAT Jaguar	15.7	4200

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
HAL HF-73	Turbo-Union RB199	15.13	9	Compare
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All data (26 fields)

Name: SEPECAT Jaguar
Manufacturer: Bréguet Aviation
Description: The SEPECAT Jaguar is a British-French supersonic jet attack aircraft originally used by the British Royal Air Force and the French Air Force in the close air support and nuclear strike role.
ICAO Code: JAGR
First Flight: 1968-09-08
Entry Into service: 1973-01-01
Production End: 1981-01-01
Service End: 2005-01-01
Designer: Bréguet Aviation
Length (m): 16.83
Height (m): 4.89
Cockpit Crew: 1
Max Speed (km/h): 1350
Max Ceiling (m): 14000
Armament: 2× 30 mm calibre DEFA cannon with up to 150 rounds/gun; 7 (4× under-wing, 2× over-wing and 1× centreline)
National Origin: France
Number Built: 573
Powerplant Description: 2 × Rolls-Royce Turbomeca Adour Mk.102 afterburning turbofan engines, 22.75 kN thrust each
Primary Users: Indian Air Force, Royal Air Force (historical); French Air Force (historical); Royal Air Force of Oman (historical)
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/SEPECAT_Jaguar
Flat Wing Span (m): 8.69
Flat Wing Area (m²): 24.18
Flat Wing Aspect Ratio: 3.12
Wake Category: M
Number of Engines: 2