Dassault Mirage 4000

The Dassault Mirage 4000 (sometimes called the Super Mirage 4000) was a French prototype jet fighter aircraft developed by Dassault-Breguet from their Mirage 2000.


Dassault Mirage 4000
Class Aircraft
Type Fighter
Manufacturer Avions Marcel Dassault-Breguet Aviation
Origin France
Country Name Origin Year
France 1979
Country Name Operational Year Retirement Year
France View
ManufacturerName Production From Production To Quantity
Avions Marcel Dassault-Breguet Aviation 1 View

The Mirage 4000 was noticeably larger and heavier than the single-engined Mirage 2000, the 4000 having two SNECMA M53-2 turbofans. It also featured small canards above the engine air intakes and a true bubble canopy compared to the Mirage 2000 and previous Mirages. Despite the changes the two aircraft remained similar, sharing the delta wing design, semi-circular air intakes and general configuration.

The Mirage 4000 first flew on 9 March 1979. It was financed as a private venture by Dassault. The Mirage 4000 was comparable in size to the United States F-15 Eagle, and was designed to be both a long-range interceptor and a capable fighter-bomber.

In the early 1980s Dassault ended the program shortly after the Saudis chose the F-15 as their preferred aircraft. The French Air Force preferred to concentrate on the Mirage 2000, leaving Dassault with no customers. Some of the expertise thus gained would later influence the Dassault Rafale. The only prototype moved to its final residence at the Musée de l'Air et de l'Espace (Paris Air and Space Museum) in 1995.

Role Prototype fighter aircraft
National origin France
Manufacturer Dassault-Breguet
First flight 9 March 1979
Status Program cancelled in the 1980s
Primary user French Air Force
Number built 1
Developed from Dassault Mirage 2000


General characteristics

  • Crew: 1
  • Length: 18.70 m (61 ft 4 in)
  • Wingspan: 12.00 m (39 ft 4 in)
  • Height: 5.80 m (19 ft 0 in)
  • Wing area: 73.0 m² (785 ft²)
  • Empty weight: 13,000 kg (29,000 lb)
  • Powerplant: 2 × SNECMA M53-2 afterburning turbofans, 95 kN (22,000 lbf) each

Performance

  • Maximum speed: 2,445 km/h (1,320 kn, 1,519 mph)
  • Range: 2,000 km (1,100 NM, 1,200 mi)
  • Service ceiling: 20,000 m (66,000 ft)

End notes