Nord 1601

Last updated
Nord 1601
Nord 1601 research aircraft in 1950.jpg
General information
TypeAerodynamic research aircraft
National originFrance
Manufacturer SNCAN, Nord Aviation
Number built1
History
First flight24 January 1950

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.

Contents

Design and development

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.

Variants

Nord 1600
Proposed fighter variant, not built.
Nord 1601
Aerodynamic research aircraft, one built.

Specifications (1601)

Data from Gaillard (1990) p.110 [1]

General characteristics

Performance

References

Bibliography