The development of the optical system for the Viking Orbiter spacecraft is presented. Each spacecraft consisted of an orbiter and a lander, and the orbiter provided support during the lander descent, landing and operation on the Martian surface, and prior to separation the orbiter provided science data for site selection and certification. To support these objectives each orbiter carried twin camera systems with identical 475 mm f/3.5 telescopes. The development of the Visual Imaging Subsystem which used all spherical catadioptric cassegrains with all elements fabricated from pure fused silica and Mangin primary mirrors is described. Computer aided design optimization and the ray aberration analysis of the final design are presented. The Viking telescopes had high theoretical and measured performance and obtained many high quality images of the Martian surface.


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    Titel :

    Optical system of the visual imaging subsystem on the Viking Orbiter spacecraft


    Beteiligte:
    Larks, L. (Autor:in)

    Kongress:

    Instrumentation in astronomy III; Seminar ; 1979 ; Tucson, AZ


    Erscheinungsdatum :

    01.01.1979


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





    The Viking Orbiter Visual Imaging Subsystem

    Wellman, J. B. / Landauer, F. P. / Norris, D. D. et al. | NTRS | 1976


    The Viking Orbiter Visual Imaging Subsystem

    John B. Wellman / Frederick P. Landauer / David D. Norris et al. | AIAA | 1976


    The Viking Orbiter Visual Imaging Subsystem

    WELLMAN, J. / LANDAUER, F. / NORRIS, D. et al. | AIAA | 1976