title: SNCAC NC.271
text: # SNCAC NC.271
  
  The SNCAC NC.271 was a French experimental aircraft built by SNCAC in the late 1940s, as a 1:2.5 scale model of the proposed SNCAC NC.270 jet bomber, featuring swept-back wings, using SNCASE SE-161 Languedoc N0.31 F-BCUT as a launch platform.
  
  ## Variants
  
  ### NC.270
  
      A proposed jet bomber, to have been powered by two Rolls-Royce Nene turbojet engines. Development was curtailed in June 1949 with the liquidation of the Aerocentre combine.
  
  ### NC.271-01
  
      A 1:2.5 scale NC.270 glider research aircraft; first free flight on 28 January 1949.
  
  ### NC.271-02
  
      A powered version of the NC.271, fitted with a 7.848 kN (1,764 lbf) Walter HWK 109-509A liquid-fuelled rocket engine; development was abandoned with the collapse of Aérocentre.
  
  ## Specifications (NC.271-01)
  
  Data from Aviafrance: NC.271, Les Avions Francais de 1944 a 1964
  
  General characteristics
  
  * Crew: One
  * Length: 8.11 m (26 ft 7 in)
  * Wingspan: 7.60 m (24 ft 11 in)
  * Height: 2.94 m (9 ft 8 in)
  * Wing area: 11.44 $m^2$ (123.1 sq ft)
  * Max takeoff weight: 1,725 kg (3,803 lb)
  
               Max Take-off weight NC.271-02: 3,400 kg (7,500 lb)
  * Powerplant: 1 × Walter HWK 109-509A liquid-fuelled rocket, 7.848 kN (1,764 lbf) thrust (NC.271-02)
  
  Performance
  
  * Maximum speed: 900 km/h (560 mph, 490 kn) (NC.271-02)
  