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Nord 1601

Supersonic and Experimental Aircraft

The Nord 1601 was a French research aircraft built by Nord Aviation to study the aerodynamics of swept wings and the high-lift devices used with them. It was a mid-wing monoplane with a wing swept at 33 degrees, fitted with ailerons, spoilers, leading edge slats and trailing edge flaps, a retractable tricycle undercarriage and a Martin-Baker ejection seat in an enclosed cockpit. Two Rolls-Royce Derwent V turbojets in underslung wing nacelles powered it. Registered F-WFKK, the single aircraft first flew on 24 January 1950. A fighter version, the Nord 1600, was proposed but never built, so the 1601 remained a one-off used purely for research.

Facts
Year
1950 1
Engine Class
Turbojet 1
Units Built
1 1
Top Speed (km/h)
1000 1
Mass (kg)
4710 1
Maximum Mass (kg)
6700 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Nord 1601 (Wikipedia)

Of Make

Source Nord 1601 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Nord 1601 (Wikipedia)Lead, maker
Quote, Lead, maker
The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation.

Originated In

Also in Geography Atlas: where this subject originated.

Source Nord 1601 (Wikipedia)Lead, origin
Quote, Lead, origin
The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation.
Sources
1. Nord 1601 (Wikipedia)
  • Design and development, first flight
    The 1601, registered F-WFKK, first flew on the 24 January 1950.
  • Design and development
    The 1601 was a cantilever mid-wing monoplane with a 33° swept wing.
  • Design and development, engines
    was powered by two Rolls-Royce Derwent V turbojets in underslung, wing mounted nacelles on either side of the fuselage
  • Specifications, empty weight
    Empty weight: 4,710 kg (10,384 lb)
  • Specifications, gross weight
    Gross weight: 6,700 kg (14,771 lb)
  • Specifications, maximum speed
    Maximum speed: 1,000 km/h (621 mph, 540 kn)
  • Variants, number built
    Aerodynamic research aircraft, one built.
  • Lead, maker
    The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation.
  • Lead, origin
    The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation.
  • Exemplifies: Aviation, Lead, mode
    The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation.
  • In Group: Experimental Jet Research Aircraft, Lead, type
    The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation.
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