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Dassault-Breguet
Mirage IV (7 pics)
Mirage IV, P, 62 C1, French Air force. At Kleine Brogel AFB Belgium November 2000
In
need for transport for their Atomic Bomb, the French Air Force brought out
specifications in 1954 for a very fast long distance bomber.
Dassault
was leading a consortium that (at first) was monitoring the development of the
Sud-Ouest S.O. 4050 Vautour, but their interest was focused in 1956 on the
possibilities of re-developing earlier studies of Dassault for a two-engine
night fighter.
These
studies led to the design of the Mirage IV, in fact an enlarged Mirage
III with two engines and possibilities to transport a 60 kiloton AN22 Glider bomb.
The
prototype flew for the first time in June 1959 thanks to the propulsion of two SNECMA
Atar 9 turbojets (59,53 kN). It proved that it could keep up speeds of Mach
2 at high altitude.
Three
pre-production aircraft were build with over the whole slightly lager measurements
and two Atar 9C turbojets (63,50 kN). The first of those three flew in
October 1961 and represented the Mirage IV A production model with a
round radar dome under de fuselage for the antenna of the bomb-aiming
radar.
The
last of the three pre-production models was fitted with Atar 9K engines,
the possibility of midair refueling and the latest navigation- and
attack-systems.
The
Mirage IV A production counted a total of 62 aircraft, twelve of those
were later converted to Mirage IV R strategic reconnaissance-aircraft
with the CT52 'Mission package' in the former bomb-bay. In the
middle of the eighties another 18 Mirage IV's were upgraded to Mirage
IV P 'Missile Carriers' They got new navigation and attack systems
and improved electronic defense systems. The Mirage IV P is designed for
penetrating enemy airspace on low altitudes as Launchers of the ASMP
missiles with nuclear warheads.
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Dassault-Breguet
Mirage IV
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Developing
Nation:
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France |
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First
Flight(s):
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June
1959 |
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Crew:
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2 |
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Wing
Span:
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11,85 m |
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Wing:
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78 m2 |
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Length:
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23,50 m |
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Weight
empty:
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14.500 kg. |
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Weight
Max. Load:
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31.600 kg. |
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Engine
(s):
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two SNECMA
Atar 09K turbojets (69,44 kN) with afterburner |
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Max.
Speed:
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2124 Kph. (Mach 2,2) at 11.000 m |
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Max.
Height:
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20.000 m |
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Max.
Range:
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1600+ (without refueling) |
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Weapons:
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- 1x one megaton nuclear bomb half sunk
under the hull |
Research
by M.v.Leeuwen
Last page update ©
zap16.com:
11-Oct-2007
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