Abstract The possibility of the spacecraft insertion into the system of operational heliocentric orbits has been analyzed. It has been proposed to use a system of several operational heliocentric orbits. On each orbit, the spacecraft makes one or more revolutions around the Sun. These orbits are characterized by a relatively small perihelion radius and relatively high inclination, which allows one to investigate the polar regions of the Sun. The transition of the spacecraft from one orbit to another has been performed using an unpowered gravity assist maneuver near Venus and does not require the cruise propulsion operation. Each maneuver transfers the spacecraft into the sequence of operational heliocentric orbits. We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). The mass of the spacecraft delivered to these systems of operational orbits has been estimated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits


    Beteiligte:
    Konstantinov, M. S. (Autor:in) / Thein, Min (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2017




    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




    Spacecraft Injection into a Heliocentric Terrestrial Orbit

    Kurt, V. G. / Sukhanov, A. A. | Springer Verlag | 2003


    Spacecraft Injection into a Heliocentric Terrestrial Orbit

    Kurt, V. G. / Sukhanov, A. A. | Online Contents | 2003


    Solar Sail Heliocentric Earth-Following Orbits

    Heiligers, Jeannette / McInnes, Colin R. | AIAA | 2015