The configuration, trajectories, and payloads of a spinning Earth-orbiting satellite designed by ESA for a post-perihelion flythrough (Giotto mission) of Comet Halley are described. Experiments approved for use on two identical three-axis stabilized Venera spacecraft destined to encounter the comet after releasing probes to Venus are listed as well as the instruments to be carried on Japan's Planet-A flyby mission. The main features launch windows are given for each spacecraft.


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    Titel :

    Plans for Comet Halley


    Beteiligte:
    Rahe, J. (Autor:in)


    Erscheinungsdatum :

    01.10.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Comet Halley and history

    Marsden, B. G. | NTRS | 1979


    Nucleus studies of Comet Halley

    Sekanina, Z. | NTRS | 1985


    The Landscape of comet Halley

    Merényi, E. | TIBKAT | 1989


    The splitting of comet Halley

    Daohan, C. / Linzhong, L. / Gilmore, A. et al. | British Library Conference Proceedings | 1998


    Nucleus studies of comet Halley

    Sekanina, Z. | Elsevier | 1985