The main objectives of the Cassini mission are to deliver a spacecraft into orbit about Saturn and a Probe into the atmosphere of Titan. Two fundamental constraints drive the design of the initial Saturn orbit and thus affect the mission performance. The first requirement is safe passage through the ring system upon Saturn arrival; the second is delivery of the Probe to Titan with an acceptable relative approach velocity. These constraints lead to the selection of a dual-burn insertion strategy, with maneuvers at periapsis and apoapsis of the initial orbit. Additional science goals constrain the Saturn arrival date and may affect the timing of the orbit insertion burn.


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    Titel :

    Saturn orbit insertion options for the Cassini mission


    Beteiligte:
    Weinstein, S. S. (Autor:in) / Stetson, D. S. (Autor:in)

    Kongress:

    AAS/AIAA Astrodynamics Conference 1989 ; 1989 ; Stowe, VT, United States


    Erscheinungsdatum :

    01.01.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Saturn orbit insertion mission plan for Cassini

    Chang, Ya-Pei Holden / Stetson, Douglas S. | NTRS | 1990


    Saturn orbit insertion mission plan for Cassini

    CHANG, YA-PEI / STETSON, DOUGLAS | AIAA | 1990


    Cassini mission to Saturn

    Spehalski, Richard J. | SPIE | 1996


    Critical Monitoring of the Cassini Saturn Orbit Insertion Maneuver

    Asmar, S.W. / Johnston, D.V. / Maize, E. et al. | AIAA | 2004


    Critical monitoring of the Cassini Saturn Orbit Insertion maneuver

    Asmar, S. W. / Johnston, D. V. / Maize, E. et al. | NTRS | 2004