""
MC.
DONNELL
Mc
        DONNELL 
      XH-20  | 
    



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         Debido al interés de la US Air Force y el US Army en un avión de alas giratorias con un rotor autopropulsado se construyeron dos prototipos que se ganarían luego el apodo de Little Henry. Consistían en una pequeña y ligera estructura en tubos de acero y un rotor de dos palas sin transmisión propulsados por un pequeño estatorreactor en cada una de las puntas de las palas. El primer vuelo se efectuó el 5 de mayo de 1947 pero tres años de pruebas confirmaron que a pesar del éxito de los vuelos, el alto consumo de combustible lo hacia completamente antieconómico.  | 
    
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         The XH-20, the world's first ram-jet helicopter, was designed to serve as a test stand for studying the feasibility of using ram-jets mounted at the tips of rotor blades for power. After preliminary engineering developments, the ram-jets were mounted on a two-bladed rotor which was subsequently mounted a welded tube structure. This structure, which served as the desired test stand, was capable of controlled free flight while carrying a pilot and was therefore classified as a helicopter. The XH-20 made a flight on May 5, 1947, but its fuel was delivered to it through a flexible line from tanks on the ground. On May 20, 1948, it made its first flight several feet off the ground while carrying self-contained fuel tanks. Being a test stand, "Little Henry" was never intended to fly at any appreciable altitudes or distances.  | 
  
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         Characteristics  | 
      
         Information  | 
      
         Characteristics  | 
      
         Information  | 
    
| First
        Flight Primer Vuelo  | 
      
         1947  | 
      Engine Motor  | 
      
          
    2 MC DONNELL  | 
    
| Seating
        Capacity Plazas  | 
      
         1  | 
      Power Potencia  | 
      
         30 HP each  | 
    
| Empty
        Weight Peso Vacío  | 
      
         290 Lb  | 
      Hover
        Ceiling O.G.E. Estacionario O.G.E  | 
      
         Ft  | 
    
| Maximum
        Weight Peso Máximo  | 
      
         Lb  | 
      Hover
        Ceiling I.G.E. Estacionario I.G.E  | 
      
         Ft  | 
    
| Vel.
        Cruise Vel. crucero  | 
      
         Kts  | 
      Service
        Ceiling Techo de Servicio  | 
      
         Ft  | 
    
| V.N.E. V.N.E  | 
      
         45 Kts  | 
      Maximum
        Range (Std) Alcance (Std)  | 
      
         NM  | 
    
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         Dimensions / Dimensiones  | 
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| Total
        Length Largo Total  | 
      
          12,33 Ft  | 
      Main
        Rotor Diameter Diam. Rotor Principal  | 
      
         20,00 Ft  | 
    
| Total
        Height Alto Total  | 
      
         6,66 Ft  | 
      Tail
        Rotor Diameter Diam. Rotor de Cola  | 
      
         NA  | 
    
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