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Sud Aviation SE-116 Voltigeur

Military Aircraft

The Sud Aviation SE-116 Voltigeur was a French twin-engined army support aircraft of the late 1950s, intended for observation, photography and ground attack. It came out of a French programme begun in 1958, during the Algerian War, for a counter-insurgency aircraft; the other contenders were the SIPA S.1100 and, slightly later, the Dassault Spirale. The Voltigeur was a low-wing cantilever monoplane with a glazed nose and cabin, tricycle landing gear with twin main wheels for rough strips, and perforated airbrakes behind the wing. The first prototype used Wright Cyclone radial engines and the second used Turbomeca Bastan turboprops. The first flight was on 5 June 1958 by Roger Carpentier, and the turboprop version flew on 15 December 1958. On 9 January 1959 tail flutter in a high-speed run killed Carpentier and two colleagues. Only three aircraft were built, and the programme was dropped without series production.

Facts
Year
1958 1
Engine Class
Piston 1
Engine Class
Turboprop 1
Status
Cancelled 1
Units Built
3 1
Top Speed (km/h)
455 1
Mass (kg)
4200 1
Maximum Mass (kg)
6520 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Sud Aviation SE-116 Voltigeur (Wikipedia)

Of Make

Source Sud Aviation SE-116 Voltigeur (Wikipedia)
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Manufactured By

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Source Sud Aviation SE-116 Voltigeur (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The twin turboprop Sud Aviation SE-116 Voltigeur

Originated In

Also in Geography Atlas: where this subject originated.

Source Sud Aviation SE-116 Voltigeur (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
was a French army support aircraft capable of observation and ground attack operations
Sources
1. Sud Aviation SE-116 Voltigeur (Wikipedia)
  • Design and development, first flight
    The piston-engined Voltigeur was first flown on 5 June 1958
  • Lead
    Three were built but no series production was undertaken.
  • Lead, body style
    The twin turboprop Sud Aviation SE-116 Voltigeur of the late 1950s was a French army support aircraft
  • Design and development, second prototype
    the Cyclones were replaced with 567 kW (760 hp) Turbomeca Bastan turboprops
  • Design and development, first prototype
    The first prototype had 597 kW (800 hp) Wright Cyclone nine cylinder radial engines
  • Specifications, empty weight
    Empty weight: 4,200 kg (9,259 lb)
  • Specifications, maximum take-off weight
    Max takeoff weight: 6,520 kg (14,374 lb) with external stores
  • Specifications, performance
    Maximum speed: 455 km/h (283 mph, 246 kn)
  • Design and development, end of programme
    the Voltigeur programme was abandoned
  • Lead, manufacturer
    The twin turboprop Sud Aviation SE-116 Voltigeur
  • Lead, country of origin
    was a French army support aircraft capable of observation and ground attack operations
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