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Sud Aviation Vautour

Military Aircraft

The Sud-Ouest S.O. 4050 Vautour, French for vulture, was a twin-jet multirole aircraft that served as a bomber, ground attack, reconnaissance and interceptor type. It was designed by SNCASO in answer to a June 1951 French Air Force requirement for a jet able to bomb, attack at low level and intercept in all weather, and was developed and built by what became Sud Aviation. The prototype first flew on 16 October 1952, and the production Vautour II, built in three variants, entered French service in 1958. The French fleet carried nuclear weapons in the strike force but never saw combat, and its lack of radar and advanced navigation equipment led to its replacement by the Dassault Mirage IV; the last frontline French aircraft were retired in 1979. Israel was the only export customer and used the Vautour in combat in the Six-Day War and the War of Attrition before replacing it with the Douglas A-4 Skyhawk in the early 1970s.

Facts
Year
1952 1
Engine Class
Turbojet 1
Status
Retired from service 1
Top Speed (km/h)
1106 1
Mass (kg)
10,000 1
Maximum Mass (kg)
21,000 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Sud Aviation Vautour (Wikipedia)

Of Make

Source Sud Aviation Vautour (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Sud Aviation Vautour (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
Developed and manufactured by aircraft company Sud Aviation

Originated In

Also in Geography Atlas: where this subject originated.

Source Sud Aviation Vautour (Wikipedia)Lead
Quote, Lead
is a French jet-powered multirole aircraft
Sources
1. Sud Aviation Vautour (Wikipedia)
  • Development, origins, first flight
    On 16 October 1952, the first prototype of the revised design, which had been designated as the S.O. 4050, conducted its maiden flight.
  • Lead
    is a French jet-powered multirole aircraft
  • Specifications, powerplant
    2 × SNECMA Atar 101E-3 turbojet engines, 34.3 kN (7,700 lbf) thrust each
  • Specifications, empty weight
    Empty weight: 10,000 kg (22,046 lb)
  • Specifications, maximum take-off weight
    Max takeoff weight: 21,000 kg (46,297 lb)
  • Specifications, performance
    Maximum speed: 1,106 km/h (687 mph, 597 kn) at sea level
  • Production and further development
    the final French aircraft being retired from frontline service during 1979
  • Lead, manufacturer
    Developed and manufactured by aircraft company Sud Aviation
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