Abstract The concepts used in the AUDIT (Assessment Using Debris Impact Theory) debris modelling suite are introduced. A sensitivity analysis is carried out to determine the dominant parameters in the modelling process. A test case simulating the explosion of a satellite suggest that at the parent altitude there is a greater probability of collision with more massive fragments.


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    Titel :

    Orbital evolution of space debris due to aerodynamic forces


    Beteiligte:
    Crowther, R. (Autor:in)

    Erschienen in:

    Advances in Space Research ; 13 , 8 ; 167-170


    Erscheinungsdatum :

    01.01.1993


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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