SNCAC NC.1071
1948
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SNCAC NC.1071

Turbojet-powered derivative of the NC.1070, the NC.1071 had enormous underwing engine nacelles, which also carried the tailfins. They were connected by a tailplane on top. The first prototype flew on 12 October 1948. The second prototype was abandoned after suffering structural damage in a flight to Mach 0.7. The project was cancelled in 1951.

3-View 
SNCAC NC.1071A three-view drawing (714 x 800)


Specification 
 ENGINE2 x 2350kg Hispano-Suiza (Rolls Royce) Nene 101
 WEIGHTS
    Take-off weight13750 kg30314 lb
    Empty weight7980 kg17593 lb
 DIMENSIONS
    Wingspan20.00 m66 ft 7 in
    Length10.75 m35 ft 3 in
    Height4.60 m15 ft 1 in
    Wing area50.00 m2538.20 sq ft
 PERFORMANCE
    Max. speed800 km/h497 mph
    Cruise speed724 km/h450 mph
    Ceiling13000 m42650 ft
    Range1000 km621 miles
 ARMAMENT2 x 20mm cannon, 800kg of weapons

Comments
Buelligan, 29.11.2014

What an odd configuration.

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