A recent development in spacecraft mission design involves the increasing use of Distributed Spacecraft Systems (DSS). Several key technologies must mature sufficiently to facilitate these missions, including the use of spacecraft flying in tightly controlled formations. Such formations may be controlled using "free flying" navigation schemes, or alternatively may use tethers to constrain the formation geometry. An investigation has been initiated here to further develop this technology using two small spacecraft connected by a short tether. After insertion into orbit, the tether will be extended and various data collected on the performance of the dual-spacecraft "formation." At some later time, the tether will be cut, and the spacecraft pair will be navigated in a manner to maintain a geometry as closely as possible to that of the tethered configuration. Comparisons and evaluations of the two modes of operation can then be made so that the merits of both approaches are available to mission designers.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design and Test of a Tethered Pair of Satellites: Equipment Requirements


    Beteiligte:

    Erscheinungsdatum :

    2003-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Tethered Communication Satellites

    Von Tiesenhausen, G. | NTRS | 1986


    Controlling short-tethered satellites

    Bschorr, O. | Elsevier | 1979



    RETRIEVAL STRATEGIES FOR TETHERED SATELLITES

    Sarego, Giulia / Bellio, Eleonora / Caon, Alex et al. | TIBKAT | 2022