Equations are developed which, for parameters of orbit inclination about moon, lunar-surface launch latitude, and stay-time on lunar surface, define plane change required to rendezvous; method of minimizing maximum plane change needed to rendezvous during stay is presented; angle of intersection between lunar departure asymptote and spacecraft satellite orbit is defined in terms of characteristics of outbound and return trajectories, orbit inclinations, and stay-times; characteristics of lunar-centered hyperbolic trajectories needed to develop equations of departure plane-change requirement are established by means of 3-dimensional joined conic analyses of Earth-moon trajectories.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Plane-change requirements associated with rendezvous in lunar satellite orbit


    Weitere Titelangaben:

    AIAA J


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 2 , n 5


    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    WHY LUNAR-ORBIT RENDEZVOUS

    Holmes, D. B. | NTRS | 1962


    Why lunar-orbit rendezvous

    Holmes, D.B. | Engineering Index Backfile | 1962


    Lunar-orbit rendezvous and manned lunar landing

    Houbolt, J.C. | Engineering Index Backfile | 1962


    Manual lunar orbit rendezvous analysis.

    Adornato, R. J. / Asbedian, V. V. / Fleisig, R. | NTRS | 1967