Dassault Mirage 4000

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Mirage 4000
Mirage 4000 prototype
Role Prototype fighter aircraft
National origin France
Manufacturer Dassault-Breguet
First flight 9 March 1979
Status Program cancelled in 1988
Primary user
French Air Force
(intended)
Number built 1
Developed from Dassault Mirage 2000
Musée de l'Air et de l'Espace
at Le Bourget, France

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

Design and development

The Mirage 4000 was noticeably larger and heavier than the single-engined Mirage 2000, the 4000 having two

SNECMA M53-2 turbofans.[1] 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-conical Oswatitsch-type air intakes, and general configuration.[citation needed
]

The Mirage 4000 first flew on 9 March 1979.

F-15 Eagle, and was designed to be both a long-range interceptor and a fighter-bomber
.

In the early 1980s, Dassault ended the program shortly after the Royal Saudi Air Force ordered a large number of Panavia Tornado aircraft. Iran had been lost as a potential customer after the Iranian Revolution in 1979.[2] 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.[3]

The prototype made a total of 336 flights, the last taking place on January 8, 1988.[4]

The only prototype moved to its final residence at the Musée de l'air et de l'espace (Paris Air and Space Museum) in November 1992.[5]

Specifications (Mirage 4000)

Data from Jane's all the World's Aircraft 1984–85,[6] Dassault Aviation[7]

General characteristics

  • Crew: 1
  • Length: 18.7 m (61 ft 4 in)
  • Wingspan: 12 m (39 ft 4 in)
  • Height: 5.8 m (19 ft 0 in)
  • Wing area: 73 m2 (790 sq ft)
  • Gross weight: 16,100 kg (35,494 lb) combat weight
  • Fuel capacity: approx 11,000 L (2,900 US gal; 2,400 imp gal) internal fuel
  • Powerplant: 2 ×
    SNECMA M53-2
    afterburning turbofan engines, 64.3 kN (14,500 lbf) thrust each dry, 95.1 kN (21,400 lbf) with afterburner

Performance

  • Maximum speed: 2,445 km/h (1,519 mph, 1,320 kn) max level speed
  • Maximum speed: Mach 2.3
  • Maximum sustained speed: M2.2
  • Approach speed: 260 km/h (160 mph; 140 kn)
  • Range: 2,000 km (1,200 mi, 1,100 nmi)
  • Combat range: 1,850 km (1,150 mi, 1,000 nmi) plus, with external tanks and recce pod
  • Service ceiling: 20,000 m (66,000 ft)
  • Rate of climb: 305 m/s (60,000 ft/min)
  • Time to altitude: 15,000 m (49,000 ft) (M2) 3 minutes
  • Wing loading: 220 kg/m2 (45 lb/sq ft) at combat weight
  • Thrust/weight: 1.2

Armament

  • Guns:
  • Hardpoints: 11 with a capacity of 8,000 kg (17,637 lb) +, with provisions to carry combinations of:
    • Other:
  • up to 3× 2,500 L (660 US gal; 550 imp gal) drop tanks
  • FLIR pod
  • Recce pod
  • laser designator pod
  • ALTIS III
  • Rockets:
  • up to 4× rocket pods
  • Missiles:
  • 2× long-range AAM
  • 8-14 advanced AAMs
  • up to 4 AGMs
  • Bombs:
  • up to 27 × 250 kg (551 lb) bombs

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

  1. ^ .
  2. ^ Mirage 4000 Origins and prototypes
  3. ^ "Mirage 4000".
  4. ^ "Dassault Super Mirage 4000 - Musée de l'Air et de l'Espace". Musée de l'Air et de l'Espace. Retrieved 2021-05-17.
  5. .
  6. ^ "Mirage 4000" (in French). Dassault Aviation. Archived from the original on 2009-02-03. Retrieved 2009-01-24.

Bibliography