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Dassault Mirage IV

Military Aircraft

The Dassault Mirage IV is a supersonic strategic bomber and deep-reconnaissance aircraft developed and produced by Dassault Aviation. Work began in the mid-1950s, when France needed a supersonic carrier for its independent nuclear deterrent, and Dassault's proposal won partly because it drew on the earlier Mirage III fighter and looked cheaper and simpler. The first prototype flew on 17 June 1959 and on 19 September 1960 set a speed record of 1,822 km/h over a 1,000 kilometre closed circuit. The first production aircraft was completed in December 1963 and the type entered French Air Force service in October 1964, where it was a vital part of the Force de Frappe. It was shifted from high-altitude to low-altitude missions in the 1960s, later carried the ASMP stand-off missile, left the nuclear role in 1996 and was withdrawn in 2005.

Facts
Year
1959 1
Engine Class
Jet 1
Status
Retired from service 1
Top Speed (km/h)
2340 1
Mass (kg)
14,500 1
Maximum Mass (kg)
33,475 1
Engine
2 × SNECMA Atar 9K-50 afterburning turbojet engines 1
Comparison
Body Style
Aircraft (no road body style) 1
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Aviation, Modes
Source Dassault Mirage IV (Wikipedia)

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Source Dassault Mirage IV (Wikipedia)
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Source Dassault Mirage IV (Wikipedia)Lead
Quote, Lead
is a supersonic strategic bomber and deep-reconnaissance aircraft developed and produced by the French aircraft manufacturer Dassault Aviation

Originated In

Also in Geography Atlas: where this subject originated.

Source Dassault Mirage IV (Wikipedia)Lead
Quote, Lead
is a supersonic strategic bomber and deep-reconnaissance aircraft developed and produced by the French aircraft manufacturer Dassault Aviation
Sources
1. Dassault Mirage IV (Wikipedia)
  • Lead
    is a supersonic strategic bomber and deep-reconnaissance aircraft developed and produced by the French aircraft manufacturer Dassault Aviation
  • Lead, year
    The first prototype, Mirage IV 01, performed its maiden flight on 17 June 1959
  • Lead, status
    the last examples of the type were withdrawn from operational service in 2005
  • Specifications
    2 × SNECMA Atar 9K-50 afterburning turbojet engines
  • Specifications, mass
    Empty weight: 14,500 kg
  • Specifications, maximum mass
    Max takeoff weight: 33,475 kg
  • Specifications, top speed
    Maximum speed: 2,340 km/h
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