The Douglas F5D Skylancer was a development of the F4D Skyray jet fighter for the United States Navy. It began as the F4D-2N, an all-weather Skyray, but the design soon became too different to count as a variation: almost every part of the airframe was modified, the fuselage was 8 feet longer and area ruled to reduce transonic drag, and the wing became much thinner. The four 20 mm cannon in the wing roots were kept, but the primary armament was to be missiles or rockets. The first flight was made by the first F5D-1 on 21 April 1956 and was supersonic. Nine test airframes were ordered with a 51-aircraft production order to follow, and four aircraft were constructed, continuing to fly in various military test programs.
Facts
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Douglas F5D Skylancer (Wikipedia)
Of Make
Source Douglas F5D Skylancer (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Douglas F5D Skylancer (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
The Douglas F5D Skylancer is a development of the F4D Skyray jet fighter for the United States Navy
Originated In
Also in Geography Atlas: where this subject originated.
Source Douglas F5D Skylancer (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
The Douglas F5D Skylancer is a development of the F4D Skyray jet fighter for the United States Navy
Sources
1. Douglas F5D Skylancer (Wikipedia)
Design and development
The first flight was made by F5D-1 (Bu. No. 139208) on 21 April 1956
Lead
F4D Skyray jet fighter
Specifications
Pratt & Whitney J57-P-8 afterburning turbojet engine
Specifications, mass
Empty weight: 17,444 lb (7,912 kg)
Specifications, maximum mass
Max takeoff weight: 31,204 lb (14,154 kg)
Lead, manufacturer
The Douglas F5D Skylancer is a development of the F4D Skyray jet fighter for the United States Navy
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