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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.

Nord 1601
Role Aerodynamic research aircraft
National origin France
Manufacturer SNCAN, Nord Aviation
First flight 24 January 1950
Number built 1

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 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


  1. Gaillard 1990, p. 110.

Bibliography



На других языках


[de] Nord 1601

Die Nord 1601 war ein französisches Forschungsflugzeug, entworfen und gebaut von Nord Aviation. Das Flugzeug wurde entwickelt, um die Aerodynamik von gepfeilten Flügeln und den dazugehörigen Hochauftriebsvorrichtungen zu untersuchen.
- [en] Nord 1601

[fr] Nord 1601

Le Nord 1601 était un avion de recherche français construit par la Société nationale des constructions aéronautiques du Nord (SNCAN), avant qu'elle ne devienne Nord-Aviation. L'avion fut conçu pour étudier l'aérodynamique des ailes en flèche et des systèmes d'augmentation de portance associés.



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