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         The work of the 
         Airborne Forces Experimental Establishment at Ringway, Manchester, on 
         the Rotachute from 1940 onwards led to the suggestion that the 
         free-wheeling autogyro principles employed could also be applied to 
         larger loads. The designer, Raoul Hafner, suggested the Rotabuggy, 
         a Jeep (or "Blitz Buggy") with rotors, and the Rotatank, 
         a similarly modified Valentine tank. A development contract was 
         placed with the M.L. Aviation Company at White Waltham in 1942, covered 
         by specification 10/42.
 Preliminary tests involved loading a Jeep with concrete and 
         dropping it from heights of up to 7 ft. 8 in. (2.35 m.), demonstrating 
         that the standard vehicle could survive undamaged from impacts of up to 
         11g. A 46 ft. 8 in. (12.4 m.) dia. two-blade rotor was then fitted, as 
         well as a streamlined tail fairing with twin rudderless fins. Other 
         additions were Perspex door panels, a 'hanging' rotor control next to 
         the steering wheel and a rotor tachometer and glider navigational 
         instruments.
 
 The Rotabuggy, camouflaged, carrying RAF roundels and a 
         prototype "P", was tow tested behind a 4½ litre supercharged Bentley, 
         and achieved gliding speeds of up to 65 mph (105 km/h) IAS.
 The first flight was made on November 16, 1943. Later, some flights 
         were made behind a Whitley bomber from Sherbourne-in-Elmet.
 
 One witness described how she watched a Whitley take off with a
         Jeep in tow, circle and land. The Jeep, still in tow, did 
         not touch down at the same time, and the witness realised that its 
         occupants "were unhappy". With the pilot holding the hanging control 
         column and the driver clutching the steering wheel, the Jeep 
         made a series of up and down movements, whilst the audience hoped it 
         would stall on a 'down' rather than an 'up'.
 
 This it fortunately did, the driver taking over and driving flat-out 
         after the Whitley, to which it remained attached. When it 
         stopped, nobody got out for a while; the pilot was then assisted out 
         and lay down beside the runway to recover. Apparently he was exhausted 
         from trying to control the joystick, which had whipped in circles for 
         the whole flight.
 
 Apparently this flight was one of the worst, and the handling and 
         flying qualities of the Rotabuggy were officially recorded as 
         "highly satisfactory", especially when large tail fins had been fitted 
         and greater rotor blade articulation provided. However, development of 
         Horsa II and Hamilcar vehicle carrying gliders made further development 
         of the idea unnecessary.
 
          
           
            | Rotabuggy data: |  
            | ROTOR SPAN: 46 ft. 8 in. (12.4 m.)
 
 GROSS WEIGHT:
 3,110 lb. (1411 kg) including
 550 lb. (241 kg) for rotor unit
 | DESIGN MAX. SPEED: 150 mph (241 km/h)
 
 EST. RATE OF DESCENT:
 960-1,980 ft/min
 (4.9-10 m/sec)
 |  |