The patent describes a laser beam pointing system, adapted for use in an aircraft. A preferred embodiment of the system includes: a laser beam source, within the aircraft, emitting a laser beam; and, a plurality of laser beam pointing devices in optical alignment with the laser beam. Each pointing device includes: a cylindrical shaped rotatable housing with a window, and either one or two rotatable optical means in optical alignment with the laser beam. This inventive system, unlike the prior art, permits the emitted laser beam to be projected over a broad range of angles with little or no aerodynamic interference with the aircraft on which it is mounted and used.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Low Drag Integration of Laser Beam Pointing Device into Aircraft


    Beteiligte:
    R. G. Gustavson (Autor:in) / D. B. Cummings (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Laser beam pointing tests

    Alley, C. O. / Currie, D. G. | NTRS | 1968


    Laser beam pointing tests

    Alley, C. O. / Currie, D. G. | NTRS | 1968


    Laser beam pointing tests

    Alley, C. O. / Currie, D. G. | NTRS | 1968


    Beam stabilization system for airborne pointing laser

    YOON YONGEUN / NAM JEONGRIM / KIM JANGPYO | Europäisches Patentamt | 2024

    Freier Zugriff