The Mars Reconnaissance Orbiter reached Mars on March 10, 2006 and performed a Mars orbit insertion maneuver of 1 km/s to enter into a large elliptical orbit. Three weeks later, aerobraking operations began and lasted about five months. Aerobraking utilized the atmospheric drag to reduce the large elliptical orbit into a smaller, near circular orbit. At the time of MRO aerobraking, there were three other operational spacecraft orbiting Mars and the navigation team had to minimize the possibility of a collision. This paper describes the daily operations of the MRO navigation team during this time as well as the collision avoidance strategy development and implementation.


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    Titel :

    Mars Reconnaissance Orbiter Aerobraking Daily Operations and Collision Avoidance


    Beteiligte:
    Long, Stacia M. (Autor:in) / You, Tung-Han (Autor:in) / Halsell, C. Allen (Autor:in) / Bhat, Ramachand S. (Autor:in) / Demcak, Stuart W. (Autor:in) / Graat, Eric J. (Autor:in) / Higa, Earl S. (Autor:in) / Highsmith, Dolan E. (Autor:in) / Mottinger, Neil A. (Autor:in) / Jah, Moriba K. (Autor:in)


    Erscheinungsdatum :

    2007-09-24


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch