Once in science mission orbits, the four 0.12-km diameter observatories plan to form a tetrahedron with as little as 4-km of separation between spacecraft. The stated operational goal of maneuvering the fleet is no more often than once every two weeks (on average). Derived maneuvering accuracy requirement levied on the ACS


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    Titel :

    Orbital Maneuvering System Design and Performance for the Magnetosperic Multiscale Formation


    Beteiligte:
    Queen, Steven (Autor:in) / Chai, Dean (Autor:in) / Placanica, Sam (Autor:in)

    Kongress:

    AAS/AIAA Astrodynamics Specialist Conference ; 2015 ; Vail, CO, United States


    Erscheinungsdatum :

    2015-08-13


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch







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