This paper presents a mathematical simulation of the initial deployment kinetics of a spacecraft solar array panel stack and its primary deployment mechanism. Two methods for achieving initial deployment are considered. The first deployment method involves the motorized deployment of a single hinge. The second deployment method involves the spring actuated deployment of two hinges. In the motorized deployment case, the solar array is predicted to slide against the spacecraft sidewall before separation. In the spring actuated deployment case, the solar array is predicted to separate from the spacecraft sidewall without sliding.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Simulation of the Initial Deployment Kinetics of a Spacecraft Solar Array


    Beteiligte:
    Burgess, S C (Autor:in)


    Erscheinungsdatum :

    01.04.1995


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Modeling and simulation of spacecraft solar array deployment

    WIE, B. / FURUMOTO, N. / BANERJEE, A. et al. | AIAA | 1986


    Modeling and simulation of spacecraft solar array deployment

    WIE, B. / FURUMOTO, N. / BANERJEE, A. K. et al. | AIAA | 1986


    Spacecraft Solar Array Deployment Analysis: A Probabilistic Approach

    Simonian, Stepan S. / Lee, Wallace T. | SAE Technical Papers | 1984


    SYSTEM FOR DEPLOYMENT OF A SOLAR ARRAY OF A SPACECRAFT

    KROON MARTIN / ROBROEK MATHIEU | Europäisches Patentamt | 2025

    Freier Zugriff