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         The 
         Fairey Rotodyne was a compound helicopter of unprecedented size at the 
         time of it's first flight on 6 Nov. 1957, having originally been 
         ordered by the then British Ministry of Supply, later the ministry of 
         Aviation, in August of 1953.  
          
         A development of the earlier Fairey Gyrodyne prototypes, which had 
         established a number of British helicopter records, the Rotodyne 
         featured a large rotor powered by air bled from two wingtip mounted 
         Napier Eland turboprops, using the rotor for vertical take-offs, 
         landings and hovering, while full power was applied to the tractor 
         propellers of the turbo props for forward flight.  
         The 
         first flight using the tractor propellers was on 10 April 1958, while 
         on January 5th 1959, the Rotodyne established a helicopter speed record 
         over a closed circuit of 307 km/h. The prototype Rotodyne was a 
         three-crew, forty-passenger machine, itself a remarkable achievement 
         for it's day but on the acquisition of Fairey, Westland Aircraft 
         proposed to develop the Rotodyne into a production aircraft capable of 
         carrying between 57 and 75 passengers and using two of the new 5,250 
         shp Rolls-Royce Tyne turboprops to give a cruising speed of 370 km/h, 
         and the ability to carry up to 6.700 Kgs of freight including 
         standard-width British Army vehicles.  
          
         However, an initial order for twelve production Rotodynes for the Royal 
         Air Force did not materialize, and after initial interest from British 
         European Airways, the state owned domestic service and European 
         international airline, did not develop into a firm order, the project 
         was abandoned in February 1962  
         
         First Flight : 
         November 6, 1957  
          
         Engines: 2 * 2.800 hp Napier Eland NEL7  
         Cruise Speed: 300 km/h  
         Range: 700 km  
         Weight: Max: 14.900 Kgs  
         Rotor Span: 27.43 m  
         Length: 17.88 m  
         Height: 6.76 m  
         Disc Area: 591 m2 
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