The BAC/Dassault AFVG, short for Anglo-French Variable Geometry, was a 1960s project for a supersonic multi-role combat aircraft with a variable-sweep wing, developed jointly by the British Aircraft Corporation in the United Kingdom and Dassault Aviation in France. The two governments agreed it on 17 May 1965, after the cancellation of the BAC TSR-2, as one of two joint projects; the other became the SEPECAT Jaguar. The specification called for Mach 2.5 at altitude and two SNECMA/Bristol Siddeley M45G turbofans. Neither Dassault nor the French Air Force was keen, and British requirements kept shifting; the French government withdrew and the project was cancelled in June 1967. BAC reworked the design as the UKVG, which led to the Anglo-German-Italian Panavia Tornado.
Facts
Engine Class Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source BAC/Dassault AFVG (Wikipedia)
Of Make
Source BAC/Dassault AFVG (Wikipedia)
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Manufactured By
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Source BAC/Dassault AFVG (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
jointly developed by British Aircraft Corporation in the United Kingdom and Dassault Aviation of France
Originated In
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Source BAC/Dassault AFVG (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
jointly developed by British Aircraft Corporation in the United Kingdom and Dassault Aviation of France
Also in Geography Atlas: where this subject originated.
Source BAC/Dassault AFVG (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
jointly developed by British Aircraft Corporation in the United Kingdom and Dassault Aviation of France
Sources
1. BAC/Dassault AFVG (Wikipedia)
Development
On 17 May 1965, following on from the cancellation of the BAC TSR-2
Development, engine class
powered by a pair of SNECMA/Bristol Siddeley M45G turbofans
Lead
project for supersonic multi-role combat aircraft
Lead, status
The project was cancelled in June 1967
Lead, manufacturer
jointly developed by British Aircraft Corporation in the United Kingdom and Dassault Aviation of France
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