An aircraft is equipped with a telescope built in the fuselage, with the initial angular mirror installed in the open part of the fuselage and the main mirror installed in the cylindrical part of the fuselage. The open part of the fuselage represents an open observation cavity with the base made of the bottom arc section of the fuselage rigidly connected with the nose of the aircraft. The main mirror is permanently fixed at the end of the cylindrical part of the fuselage at the tail. The initial angular mirror is rotary fixed to the nose. The axis of rotation of the initial angular mirror overlaps the longitudinal axis of the aircraft and the optical axis of the main mirror. The bottom arc section of the fuselage has a recess for observation of the earth, and the lifting surface is releasably fixed to the cylindrical part of the fuselage .


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    Titel :

    Aircraft for Performing Observations in the Stratosphere


    Beteiligte:
    ZURAWSKI RAFAL (Autor:in)

    Erscheinungsdatum :

    2022-04-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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