Dassault Mirage 2000

Length
14.36 m
Flat Wing Span
9.13 m
Height
5.2 m
Flat Wing Area
41 m²
Max Speed
2336 km/h
Max Ceiling
17060 m
Number of Engines
1
First Flight
1978-03-10
Entry Into service
1984-07-01
Number Built
601
Maximum Take-Off Weight
17 t (paragliders: kg)
Total Fuel Capacity
3950
Maximum Range
1550 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Dassault Mirage 2000 17 3950 1550

Similar airplanes

All data (26 fields)
Name
Dassault Mirage 2000
Manufacturer
Dassault Aviation
Description
The Dassault Mirage 2000 is a multirole, single-engine, delta wing, fourth-generation jet fighter designed and produced by the French aircraft manufacturer Dassault Aviation.
ICAO Code
MIR2
First Flight
1978-03-10
Entry Into service
1984-07-01
Production End
2007-01-01
Designer
Dassault Aviation
Type
Multirole fighter aircraft
Length (m)
14.36
Height (m)
5.2
Cockpit Crew
1
Max Speed (km/h)
2336
Max Ceiling (m)
17060
Rate of Climb (m/s)
285
Armament
2× 30 mm DEFA 554 revolver cannon, 125 rounds per gun; ; Unguided:; Mk.82; Guided:; PGM 500 and PGM 2000 modular guided bombs (Mirage 2000-9); 2 × AS-30L laser-guided missile (Mirage 2000 D); 2 × GBU-12 laser-guided bombs (Mirage 2000 D, Mirage 2000 C & Mirage 2000 N with external laser designation); 1 × GBU-16 laser-guided bomb (Mirage 2000 D, Mirage 2000 C & Mirage 2000 N with external laser de…
National Origin
France
Number Built
601
Powerplant Description
1 × SNECMA M53-P2 afterburning turbofan engine, 64.3 kN thrust each
Primary Users
French Air and Space Force, United Arab Emirates Air Force , Republic of China Air Force , Indian Air Force
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Dassault_Mirage_2000
Flat Wing Span (m)
9.13
Flat Wing Area (m²)
41
Wake Category
M
Number of Engines
1