BAC.221
research aircraft
1964

     
   
     

 

     
   
     

Test aircraft modified from F.D.2 to test the delta wing of the "Concorde". The first flight was on May 1, 1964.

Crew: 1
Engine: 1 x 5000kg
Wingspan: 7.6m
Length: 17.6m		 Wing area: 46m2
Start mass: 9000kg
Max speed: 1700kph

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