Trajectory design of the orbit phase of the NEAR mission involves a new process that departs significantly from those procedures used in previous missions. In most cases, a precise spacecraft ephemeris is designed well in advance of arrival at the target body.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Near Earth Asteroid Rendezvous (NEAR) Revised Eros Orbit Phase Trajectory Design


    Beteiligte:
    McADams, J. (Autor:in) / Farquhar, R. (Autor:in) / Dunham, D. (Autor:in) / Willimas, B. (Autor:in) / Carranza, E. (Autor:in) / Antreasian, P. (Autor:in) / Miller, J. (Autor:in) / Helfrich, C. (Autor:in)

    Erscheinungsdatum :

    1999-08-16


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Near Earth Asteroid Rendezvous (NEAR) Revised Eros Orbit Phase Trajectory Design

    Helfrich, J / Miller, J. K. / Antreasian, P. G. et al. | NTRS | 1999


    Near Earth Asteroid Rendezvous (NEAR) Revised Eros Orbit Phase Trajectory Design

    J. Helfrich / J. K. Miller / P. G. Antreasian et al. | NTIS | 1999


    Near Earth Asteroid Rendezvous Orbit Phase Trajectory Design

    Miller, J. / Carranza, E. / Helfrich, C. et al. | British Library Conference Proceedings | 1998


    Near Earth Asteroid Rendezvous orbit phase trajectory design

    Miller, J. / Carranza, E. / Helfrich, C. et al. | AIAA | 1998


    Near Earth Asteroid Rendezvous Orbit Phase Trajectory Design

    McAdams, J. / Guo, Y. / Farquhar, R. et al. | NTRS | 1998