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Dassault Super Mystere

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The Dassault Super Mystère was a French fighter-bomber, the first Western European supersonic aircraft to enter mass production.


The Super Mystère represents the final step in evolution which began with the Dassault Ouragan and progressed through the Mystère II/III and Mystère IV. While earlier Mystère variants could attain supersonic speeds only in a dive, the Super Mystère could exceed the speed of sound in level flight. This was achieved thanks to the new thin wing with 45° of sweep (compared with 41° of sweep in the Mystère IV and only 33° in Mystère II) and the use of an afterburner-equipped turbojet engine.

The first prototype Super Mystère B.1, powered by a Rolls-Royce Avon RA.7R, took to the air on March 2, 1955. The aircraft broke the sound barrier in level flight the following day. The aircraft entered production in 1957 as the Super Mystère B.2. The production version differed from the prototype by having a more powerful SNECMA Atar 101G engine. In 1958, two Super Mystère B.4 prototypes were built. Equipped with a new 48° swept wing and a more powerful SNECMA Atar 9B engine, the aircraft were capable of Mach 1.4. Production never materialized because the faster Dassault Mirage III was entering service. In 1973, the Israeli Air Force upgraded their Super Mystère B.2s with a non-afterburning version of the Pratt & Whitney J52-P8A and new avionics.

A total of 180 Super Mystère B.2s were built.

Operational history

The Super Mystère served with the French Air Force until 1977. In addition, 36 aircraft were sold to the Israeli Air Force in 1958. The aircraft saw action in the 1967 Six-Day War and the 1973 Yom Kippur War. They were well-liked by the Israeli pilots and were a match for the Arab MiG-19 aircraft in air-to-air combat.

In 1976, Israel sold 12 complete airframes to Honduras. In 1979, 4 more complete airframes were purchased by the Hondurans, totaling 16 aircraft. They were involved in numerous border skirmishes with Sandinista Nicaragua and were finally withdrawn from service in 1996 replaced by 12 Northrop F-5Es. The 11 surviving aircraft are for sale as surplus and 1 more is preserved at the Honduras Air Museum.


File:Two Super Mystère B.2 jets.JPEG
TwoSuper Mystere B.2 aircraft of the Honduran Air Force (1988)

Specifications (Super Mystère B.2)

General characteristics

  • Crew: 1
  • Length: 14.13 m (46 ft 4 in)
  • Wingspan: 10.51 m (34 ft 6 in)
  • Height: 4.6 m (15 ft 1 in)
  • Wing area: 32.0 m² (344 ft²)
  • Empty weight: 6,390 kg (14,090 lb)
  • Loaded weight: 9,000 kg (20,000 lb)
  • Max takeoff weight: 10,000 kg (22,000 lb)
  • Fuel capacity: 2,000 kg (4,400 lb)
  • Powerplant:SNECMA Atar 101G-2 turbojet
    • Dry thrust: 33.3 kN (7,490 lbf)
    • Thrust with afterburner: 44.1 kN (9,920 lbf)



See also

Related development

Comparable aircraft

Related lists


  • Donald, David; Lake, Jon (editors) (1996). Encyclopedia of world military aircraft. AIRtime Publishing. ISBN 1-880-58824-2. 
  • Kopenhagen, W. (editor) (1987). Das große Flugzeug-Typenbuch. Transpress. ISBN 3-344-00162-0.  (Written in German) Template:Dassault aircraft

de:Dassault Super Mystère es:Dassault Super Mystère fr:Dassault Super Mystère B2 it:Dassault Super Mystère he:דאסו סופר מיסטר ms:Dassault Super Mystère ja:シュペルミステール (航空機) pl:Dassault Super Mystère ru:Dassault Super Mystère sl:Dassault Super Mystère vi:Dassault Super Mystère

This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "Dassault Super Mystere".