Effort performed to identify a low cost maneuver strategy is summarized. The strategy provides a great advantage with respect to the total delta-V required for a period of one year. According to a preliminary analysis a small satellite can be conceived to support high inclined orbit missions, being the expected resulting propellant mass for a lifetime of 7 years of about 4 kg.


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    Titel :

    Low Cost Station Keeping Maneuvers for a Small-Satellites Constellation in Tundra Orbits


    Beteiligte:
    A. Cramarossa (Autor:in) / G. Barresi (Autor:in) / G. Rondinelli (Autor:in) / F. Graziani (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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