Abstract This paper presents results of an investigation into the particular features of sun synchronous orbits, and enhancements required to more accurately estimate the probability of Collision (PC). The approach taken here is to compare PC estimates using “typical” input values with “enhanced” input values specific to the sun synchronous case. The meteorological satellite NOAA-12 is used as an example. Results suggest that the collision probability for NOAA-12 using “enhanced” values is larger than the “typical” value by a factor of about 5.


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    Titel :

    Collision risk in sun synchronous low Earth orbit


    Beteiligte:
    Dittberner, G. (Autor:in) / McKnight, D. (Autor:in)

    Erschienen in:

    Advances in Space Research ; 13 , 8 ; 187-190


    Erscheinungsdatum :

    1993-01-01


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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