The Voyager spacecraft magnetometer experiment utilizes two sensors on a deployable boom. The boom is an Astromast. The implementation of the Astromast into the Voyager design is described along with the hardware used to hold, latch, and deploy the mast and the tests to demonstrate damping, deployment, and alignments. Several problems encountered are discussed and their solutions are given. Flight deployment and preliminary alignment results are presented. Finally, the design is evaluated in retrospect.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The Voyager magnetometer boom


    Beteiligte:
    Miller, D. C. (Autor:in)


    Erscheinungsdatum :

    1979-04-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    The Galeleo spacecraft magnetometer boom

    Packard, D. T. / Benton, M. D. | NTRS | 1985


    Voyager

    Hearth, D.P. | Engineering Index Backfile | 1965


    Swarm Deployable Boom Assembly (DBA) Development of a Deployable Magnetometer Boom for the Swarm Spacecraft

    McMahon, P. / Jung, H.-J. / Edwards, J. | British Library Conference Proceedings | 2013


    Voyager

    Yeager, Jeana ;Rutan, Dick ;Patton, Phil | SLUB | 1987