Abstract The problem of optimization of the interplanetary trajectory of flight for a multistage spacecraft with high- and low-thrust engines into the Jupiter satellite orbit is considered. Low-thrust engines (stationary plasma engines) are used on a heliocentric flight segment. Their operation is maintained with electric power supply from solar batteries. The principal feasibility of the realization of such a project is shown, and estimations of the mass of a spacecraft placed into Jupiter's satellite orbit are presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Use of a Solar Electrojet Propulsion System for Jupiter Satellite Injection


    Beteiligte:
    Konstantinov, M. S. (Autor:in) / Popov, G. A. (Autor:in) / Fedotov, G. G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2002




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :

    Klassifikation :

    BKL:    55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung
    Lokalklassifikation TIB:    770/3520/8000



    The Use of a Solar Electrojet Propulsion System for Jupiter Satellite Injection

    Konstantinov, M. S. / Popov, G. A. / Fedotov, G. G. | Springer Verlag | 2002



    Alfven propulsion at Jupiter

    Gabriel, S. B. / Jones, R. M. / Garrett, H. B. | NTRS | 1988


    Solar Electric Propulsion Gravity-Assist Tours For Jupiter Missions

    Strange, Nathan / Landau, Damon / Hofer, Richard et al. | AIAA | 2012


    Development of the Jupiter Propulsion System

    Braun, J. H. / Internautical Academy of Astronautics / International Astronautical Federation | British Library Conference Proceedings | 1997