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Contents

   



(Top)
 


1 Design and development  





2 Variants  





3 Specifications (1601)  





4 References  





5 Bibliography  














Nord 1601






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From Wikipedia, the free encyclopedia
 


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.

Design and development[edit]

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[edit]

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

Specifications (1601)[edit]

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

General characteristics

Performance

References[edit]

  1. ^ Gaillard 1990, p. 110.

Bibliography[edit]


Retrieved from "https://en.wikipedia.org/w/index.php?title=Nord_1601&oldid=1112256243"

Categories: 
1950s French experimental aircraft
Nord aircraft
Twinjets
Mid-wing aircraft
Aircraft first flown in 1950
Hidden categories: 
Articles with short description
Short description matches Wikidata
Short description is different from Wikidata
Commons category link is on Wikidata
CS1 French-language sources (fr)
 



This page was last edited on 25 September 2022, at 12:22 (UTC).

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