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
Engine Class Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Sud Aviation SE-116 Voltigeur (Wikipedia)
Of Make
Source Sud Aviation SE-116 Voltigeur (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Sud Aviation SE-116 Voltigeur (Wikipedia)Lead, manufacturerQuote, 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 originQuote, 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
View the SourceReader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.
Sign in to dispute this or suggest a correction.