Nord 1601
In the following article the issue of Nord 1601 will be addressed, which is a matter of utmost importance and relevance today. Nord 1601 is a topic that has aroused the interest and attention of a large number of people around the world, and its impact extends to various areas of daily life. Along these lines, different aspects related to Nord 1601 will be analyzed, providing detailed and updated information to deepen your understanding. In addition, various points of view and opinions of experts in the field will be explored, with the aim of offering a broad and enriching perspective on Nord 1601.
| 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
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
- Crew: 1
- Length: 11.62 m (38 ft 7 in)
- Wingspan: 12.40 m (40 ft 10.5 in)
- Height: 3.67 m (12 ft 0 in)
- Wing area: 30.2 m2 (333 sq ft)
- Empty weight: 4,710 kg (10,384 lb)
- Gross weight: 6,700 kg (14,771 lb)
- Powerplant: 2 × Rolls-Royce Derwent V turbojet , 17.8 kN (4,000 lbf) thrust each
Performance
- Maximum speed: 1,000 km/h (621 mph, 540 kn)
- Range: 1,135 km (705 mi, 613 nmi)
- Service ceiling: 12,000 m (39,370 ft)
References
- ^ Gaillard 1990, p. 110.
Bibliography
- Buttler, Tony & Delezenne, Jean-Louis (2012). X-Planes of Europe: Secret Research Aircraft from the Golden Age 1946-1974. Manchester, UK: Hikoki Publications. ISBN 978-1-902-10921-3.
- Cuny, Jean (1989). Les avions de combat français, 2: Chasse lourde, bombardement, assaut, exploration [French Combat Aircraft 2: Heavy Fighters, Bombers, Attack, Reconnaissance]. Docavia (in French). Vol. 30. Ed. Larivière. OCLC 36836833.
- Gaillard, Pierre (1990). Les Avions Francais de 1944 à 1964 [French Aircraft from 1944 to 1964] (in French). Paris: Éditions EPA. ISBN 2-85120-350-9.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.