A turbojet-powered derivative of the NC.1070, the NC.1071 had underwing engine nacelles, which also carried the tailfins, connected by a tailplane on top. The first prototype flew on 12 October 1948 but the second prototype was abandoned after suffering structural damage in a flight to Mach 0.7. Aerocentre went into liquidation during 1949 and the project was cancelled in 1951.
Engine: 2 x 2350kg Hispano-Suiza (Rolls Royce) Nene 101
Take-off weight: 13750 kg / 30314 lb
Empty weight: 7980 kg / 17593 lb
Wingspan: 20.0 m / 66 ft 7 in
Length: 10.75 m / 35 ft 3 in
Height: 4.6 m / 15 ft 1 in
Wing area: 50.0 sq.m / 538.20 sq ft
Max. Speed: 800 km/h / 497 mph
Cruise speed: 724 km/h / 450 mph
Ceiling: 13000 m / 42650 ft
Range: 1000 km / 621 miles
Armament: 2 x 20mm cannon, 800kg of weapons
All Aero 