The Saturn-bound Cassini spacecraft performs trajectory correction maneuvers using either the 0.6 N Hydrazine thrusters of the reaction control system (RCS) or one of the two gimbaled 490 N bipropellant main engines.


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    Title :

    Attitude Control of the Cassini Spacecraft During Propulsive Maneuvers


    Contributors:

    Publication date :

    1993-08-16


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




    Attitude Control of the Cassini Spacecraft During Propulsive Maneuvers

    Enright, P. J. / American Astronautical Society / AIAA | British Library Conference Proceedings | 1993




    Attitude Control For The Cassini Spacecraft

    Wong, Edward C. / Breckenridge, William G. / Rasmussen, Robert et al. | NTRS | 1995