The Fokker/Republic D.24 was a supersonic variable-sweep wing concept aircraft designed from 1962 to 1968 by the Fokker-Republic Alliance, a coalition between Fokker and Republic Aviation. The project was based at Schiphol in the Netherlands and led by Alexander Wadkowski of Republic Aviation. The D.24 was designed to be capable of vertical take-off and landing and in accordance with NATO Basic Military Requirement 3, and it competed in NATO's BMR-3 bidding. It was to have a single crew member and one Bristol Siddeley BS.100 vectored-thrust turbofan engine for lift and cruise, with a design maximum speed of Mach 1.5 at sea level and Mach 2.4 at 70,000 feet and a range of 4,828 km. Only a scale model was built, and it is now kept at the Aviodrome aviation museum in Lelystad in the Netherlands.
Facts
Engine Class StatusDesign only (never built) 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Fokker/Republic D-24 Alliance (Wikipedia)
Of Make
Source Fokker/Republic D-24 Alliance (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Fokker/Republic D-24 Alliance (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
The Fokker/Republic D.24 was a supersonic variable-sweep wing concept aircraft designed from 1962 to 1968 by the Fokker-Republic Alliance
Originated In
Also in Geography Atlas: where this subject originated.
Source Fokker/Republic D-24 Alliance (Wikipedia)Lead, country of originQuote, Lead, country of origin
The project was based out of Schiphol, Netherlands
Sources
1. Fokker/Republic D-24 Alliance (Wikipedia)
Lead
Only a scale model was built
Lead, engine class
Bristol Siddeley BS.100 vectored-thrust turbofan engine
Lead, body style
supersonic variable-sweep wing concept aircraft
Lead, manufacturer
The Fokker/Republic D.24 was a supersonic variable-sweep wing concept aircraft designed from 1962 to 1968 by the Fokker-Republic Alliance
Lead, country of origin
The project was based out of Schiphol, Netherlands
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