The hazard to mission operations posed by space debris in Geostationary Transfer Orbit (GTO) is considered. A number of debris mitigation strategies are considered. These include the harnessing of the luni-solar perturbation to the satellite orbit, atmospheric drag augmentation, and active propulsive deorbit. Results suggest that active deorbit using a dedicated propulsive unit offers the least performance penalty.


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    Titel :

    Limitation of Space Debris in Geostationary Transfer Orbit


    Beteiligte:
    R. Crowther (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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