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Contents

   



(Top)
 


1 Design and development  





2 Specifications  





3 References  





4 Bibliography  














SNCASE SE-2100






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SE-2100
Role Two seat experimental tailless pusher touring aircraft
National origin France
Manufacturer Sud-Est (Société nationale des constructions aéronautiques du Sud-Est or SNCASE)
Designer Pierre Satre
First flight 4 October 1945
Number built 1

The Sud-Est or SNCASE SE-2100, sometimes known as the Satre SE-2100 after its designer, was a tailless, pusher configuration touring monoplane with a single engine and cabin for two. Only one was built.

Design and development[edit]

The SE-2100 was designed by Pierre Satre,[1][2] later the chief designer of the Concorde,[citation needed] as a response to a 1943 specification by the Vichy French Air Ministry for a two-seat touring aircraft.[2] An all-metal aircraft, it had a low, cantilever, straight tapered wing with 55° of sweep on the leading edge and 10.43° of dihedral. There were fixed leading edge slots and trailing edge ailerons but no conventional flaps. The wing tips carried large, rounded fins with rudder-like rear portions which only moved outwards; they were used differentially for yaw control and jointly as flaps.[3]

The SE-2010 had a short, blunt-nosed nacelle-type fuselage with a cabin which could be configured to seat one centrally or two in side-by-side, dual control configuration. The seats were just aft of the leading edge, with a baggage compartment behind them. Access was via deep, wide, forward hinged doors on both sides; to make this possible, a piece of the wing root leading edge was an integral part of each door. A 140 hp (104 kW) Renault Bengali 4 four cylinder, inverted, inline engine was mounted in pusher configuration behind the cabin and air-cooled via a ventral scoop; it drove a two-blade propeller positioned just behind the trailing edge. The SE-2100's fixed, tricycle undercarriage had pneumatic shock absorbers and mainwheel brakes; the nosewheel was free-swivelling.[3] At different times the undercarriage legs and wheels were unfaired or faired.[1]

The SE-2010 flew for the first time on 4 October 1945.[4] Despite demonstrating promising performance[5] and showing high manoeuvrability when demonstrated at the 1946 Paris Air Show,[6] no production followed, with the prototype surviving into the early 1950s.[7]

Specifications[edit]

Data from Jane's All the World's Aircraft 1948[3]

General characteristics

Performance

References[edit]

  1. ^ a b "Satre SE-2100". T.W.I.T.T. (The Wing is the Thing). Archived from the original on 14 April 2021. Retrieved 16 November 2012.
  • ^ a b de Narbonne 2005, pp. 70–71
  • ^ a b c Bridgman 1948, pp. 159c–160c
  • ^ de Narbonne 2005, p. 70
  • ^ Pelletier 1996, p. 11
  • ^ de Narbonne 2005, p. 73
  • ^ de Narbonne 2005, pp. 70, 73
  • Bibliography[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=SNCASE_SE-2100&oldid=1181352423"

    Categories: 
    1940s French experimental aircraft
    SNCASE aircraft
    Sud-Est aircraft
    Single-engined pusher aircraft
    Tailless aircraft
    Aircraft first flown in 1945
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    All articles with unsourced statements
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    Aircraft specs templates using more performance parameter
    Commons category link is on Wikidata
    CS1 French-language sources (fr)
     



    This page was last edited on 22 October 2023, at 14:48 (UTC).

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