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| 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.
 | A three-view drawing (714 x 800) |
| ENGINE | 2 x 2350kg Hispano-Suiza (Rolls Royce) Nene 101 |
| WEIGHTS |
| Take-off weight | 13750 kg | 30314 lb |
| Empty weight | 7980 kg | 17593 lb |
| DIMENSIONS |
| Wingspan | 20.00 m | 66 ft 7 in |
| Length | 10.75 m | 35 ft 3 in |
| Height | 4.60 m | 15 ft 1 in |
| Wing area | 50.00 m2 | 538.20 sq ft |
| PERFORMANCE |
| 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 |
| Buelligan, e-mail, 29.11.2014 09:09 What an odd configuration. reply |
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