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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Plans for Comet Halley


    Beteiligte:
    Rahe, J. (Autor:in)


    Erscheinungsdatum :

    1981-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Nucleus studies of comet Halley

    Sekanina, Z. | Elsevier | 1985


    The splitting of comet Halley

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


    Comet Halley observations to date

    Rahe, Jürgen | Elsevier | 1984


    EUV observations of Comet Halley

    Ripken, H.W. / Fahr, H.J. / Lay, G. | Elsevier | 1984