| Nord 1601 | |
|---|---|
 | |
| Role | Aerodynamic research aircraft |
| National origin | France |
| Manufacturer | SNCAN, Nord Aviation |
| First flight | 24 January 1950 |
| Number built | 1 |
The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation. The aircraft was designed to investigate the aerodynamics of swept wings and related high-lift devices.
The 1601 was a cantilever mid-wing monoplane with a 33° swept wing. The wing was fitted with ailerons, spoilers, leading edge slats and trailing edge flaps. It had retractable tricycle landing gear and was powered by two Rolls-Royce Derwent V turbojets in underslung, wing mounted nacelles on either side of the fuselage. It had an enclosed cockpit and was fitted with a Martin-Baker ejection seat. The 1601, registered F-WFKK, first flew on the 24 January 1950.
Data from Gaillard (1990) p.110 [1]
General characteristics
Performance
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