{"id":4519,"date":"2025-04-10T22:28:17","date_gmt":"2025-04-10T19:28:17","guid":{"rendered":"https:\/\/adifoaircraft.com\/fly\/?page_id=4519"},"modified":"2025-04-11T13:15:37","modified_gmt":"2025-04-11T10:15:37","slug":"adifo","status":"publish","type":"page","link":"https:\/\/adifoaircraft.com\/fly\/?page_id=4519","title":{"rendered":"ADIFO"},"content":{"rendered":"

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PROJECTS<\/span>ADIFO<\/span><\/span><\/h1>
VTOL aicraft able to fly in all directions

\nhaving the same aerodynamic characteristics.

\nThe only limit is the pilot's imagination...<\/div><\/header><\/div><\/div><\/div><\/div><\/div><\/div><\/div><\/div>
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All directions
\nflying object<\/h1>\n

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ADIFO, a game-changer in aerospace innovation – leverages Dolphin Profiles for exceptional aerodynamic versatility. Its circular design and unique propulsion system enable unprecedented maneuverability and efficiency.<\/p>\n

A groundbreaking platform utilizing revolutionary aerodynamics for extremely high speeds (including supersonic) with exceptional maneuverability. Its VTOL capabilities ensure unmatched stability and control, making itideal for advanced aerospace applications, both civil and military.<\/p>\n

\n<\/div><\/div><\/div><\/div><\/div><\/div>

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Unique Configuration<\/h1>\n

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  • As a circular shape
    \nand thefuselage is alsoa wing
    \n<\/strong>_______________________________________<\/li>\n
  • The aerodinamic body <\/strong>
    \nis axial symmetric.<\/strong>
    \n_______________________________________<\/li>\n
  • And is obtained by rotating <\/strong>
    \na biderictional Dolphin airfoil, <\/strong>
    \naround the axis perpendicular <\/strong>
    \non the midle of the chord line.<\/strong>
    \n_______________________________________<\/li>\n<\/ul>\n

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    Features<\/h1>\n

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    • The first aircraft in the world capable of easily reaching supersonic speeds while also flying well at low speeds.<\/strong>
      \n_______________________________________<\/li>\n
    • The first aircraft in the world capable of performing abrupt rotations and translations at very high speeds.<\/strong>
      \n_______________________________________<\/li>\n
    • Capable of generating random, non-extrapolatable trajectories and, consequently, impossible to intercept by current anti-aircraft systems.<\/strong>
      \n_______________________________________<\/li>\n<\/ul>\n

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      Aerodynamicity<\/h1>\n

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      Tested at lowspeed in the wind tunnel.
      \nConclusion: Smooth transition from subsonic to supersonic flight!<\/h6>\n

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      • High lift\/drag ratio<\/li>\n
      • Wide range of useful incidence angles (even over 60 degrees)<\/li>\n
      • Uniform distribution of aerodynamic load<\/li>\n
      • No stagnation points<\/li>\n
      • No sonic boom<\/li>\n
      • Low vibrations<\/li>\n
      • Low heating<\/li>\n
      • Low aerodynamic noise<\/li>\n
      • High fuel economy at encreased speeds<\/li>\n<\/ul>\n

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        Hyper maneuverability<\/h1>\n

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        • Vectored nozzles for cruise maneuvers (yaw, roll & pitch)
          \n________________________________<\/li>\n
        • Reaction control system with lateral and vertical nozzles
          \n________________________________<\/li>\n
        • Sudden lateral translations and sudden yaw
          \n________________________________<\/li>\n
        • Combined maneuvers in any directions at high speeds
          \n________________________________<\/p>\n
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          The only limit of maneuvrability
          \nis the pilot’s imagination<\/h6>\n

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          Uses<\/h1>\n

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          • Personal aircraft
            \n______________________________<\/li>\n
          • Unmanned aerial vehicle (UAV)
            \n______________________________<\/li>\n
          • Unmanned aerial combat vehicle (UCAV)
            \n______________________________<\/li>\n
          • Fighter aircraft Missiles
            \n______________________________<\/li>\n
          • Fast loitering munition
            \n______________________________<\/li>\n
          • Suborbital \/ Orbital vehicle
            \n______________________________<\/li>\n<\/ul>\n

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            ADIFO Patents<\/h3>\n

            Granted patents:
            \nEPO, US, EAPO, JP, RO, CA, IL, IN, CN<\/h6>\n

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