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Vought F-8E(FN) Crusader

Military Aircraft

The Vought F-8E(FN) Crusader was a variant of the Vought F-8 Crusader built solely for the French Navy's air arm, the Aeronavale, as a fleet air defence fighter. France needed a modern interceptor for the new carriers Clemenceau and Foch, and after deck trials in 1962 the Crusader was chosen over the larger McDonnell F-4 Phantom. The order was for 42 single-seat aircraft, the last Crusaders ever built. To fly from the smaller French decks the F-8E was modified to land about 15 knots slower: the incidence of the variable-incidence wing was reduced from 7 to 5 degrees, boundary layer control was added, and the tail area and leading edge slats were enlarged. French aircraft could carry the R.530 missile as well as the Sidewinder, and used an improved radar, the AN/APQ-104. The type entered service in 1964, was upgraded in the late 1980s and was withdrawn in December 1999.

Facts
Year
1964 1
Engine Class
Turbojet 1
Status
Retired from service 1
Units Built
42 1
Top Speed (km/h)
1609 1
Mass (kg)
8960 1
Maximum Mass (kg)
15,420 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Vought F-8E(FN) Crusader (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Vought F-8E(FN) Crusader (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The F-8E(FN) is a variant of the Vought F-8 Crusader
Sources
1. Vought F-8E(FN) Crusader (Wikipedia)
  • Lead
    The F-8E(FN) is a variant of the Vought F-8 Crusader operated exclusively by the French Navy's air arm, the Aéronavale, in the fleet air defence role.
  • Lead, service entry
    Entering service in 1964, the Crusader underwent a major upgrade in the late 1980s
  • Lead, status
    The Crusader was eventually withdrawn in December 1999.
  • Background
    leading to France's order being amended to 42 single-seat aircraft
  • Specifications
    Powerplant: 1 × Pratt & Whitney J57-20A axial-flow turbojet
  • Specifications, mass
    Empty weight: 19,751 lb (8,960 kg)
  • Specifications, maximum mass
    Max takeoff weight: 34,000 lb (15,420 kg)
  • Specifications, top speed
    Maximum speed: 1,000 mph (1,609 km/h, 870 kn) at altitude
  • Lead, manufacturer
    The F-8E(FN) is a variant of the Vought F-8 Crusader
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