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to low-altitude missions in the 1960s, later carried the ASMP stand-off missile, left the nuclear role in 1996 and was withdrawn in 2005.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
Engine Class Top Speed (km/h) Maximum Mass (kg) Engine2 × SNECMA Atar 9K-50 afterburning turbojet engines 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Dassault Mirage IV (Wikipedia)
Of Make
Source Dassault Mirage IV (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Dassault Mirage IV (Wikipedia)LeadQuote, 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)LeadQuote, 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the last examples of the type were withdrawn from operational service in 2005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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